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Langley Research Center

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• Langley Research Center: A Computer Program for the Determination of the Acoustic Pressure Signature of Helicopter Rotors Due to Blade Thickness (NASA Technical Memorandum X-3323; 1976), also by Gerald H. Mall and F. Farassat (page images at HathiTrust)

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Additional books from the extended shelves:

• Langley Research Center: 14th Aerospace Mechanisms Symposium: Proceedings of a symposium sponsored by National Aeronautics and Space Administration, the California Institute of Technology, and Lockheed Missiles and Space Company Inc.,and held at NASA Langley Research Center, Hampton, Virginia. (NASA Scientific and Technical Information Office, 1980), also by Aerospace Mechanisms Symposium (14th : 1980 : Langley Research Center), United States. National Aviation Administration, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Lockheed Aircraft Corporation, and California Institute of Technology (page images at HathiTrust)
• Langley Research Center: 1975 Ride Quality Symposium, held at Williamsburg, Virginia, August 11-12, 1975. (National Aeronautics and Space Administration ;, 1975), also by Va.) Workshop on Vehicle Ride Quality (1975 : Williamsburg, United States. Dept. of Transportation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: 1980 Aircraft safety and operating problems : proceedings of a NASA conference held at Langley Research Center, Hampton, Virginia, November 5-7, 1980 (National Aeronautics and Space Administration, Scientific and Technical Information Office :, 1981), also by Joseph W. Stickle, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and NASA Aircraft Safety and Operating Problems Conference (1980 : Langley Research Center.) (page images at HathiTrust)
• Langley Research Center: 1989 high-speed civil transport studies (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Douglas Aircraft Company. HSCT Concept Development Group (page images at HathiTrust)
• Langley Research Center: 1991 International Conference on Aging Aircraft and Structural Airworthiness : proceedings of an international conference sponsored by the Federal Aviation Administration and the National Aeronautics and Space Administration, Washington, D.C., and held in Washington, D.C., November 19-21, 1991 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by D.C.) International Conference on Aging Aircraft and Structural Airworthiness (1991 : Washington, Charles E. Harris, United States National Aeronautics and Space Administration, and United States Federal Aviation Administration (page images at HathiTrust)
• Langley Research Center: 4D-TECS integration for NASA TSRV airplane (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by I. Kaminer, P. R. O'Shaughnessy, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: 60 GHz radiometric local vertical sensor experiment (National Aeronautics and Space Administration ;, 1973), also by C. Herbert Grauling and Westinghouse Defense and Electronics Systems Center (page images at HathiTrust)
• Langley Research Center: Ablation performance of glasslike carbons, pyrolytic graphite, and artificial graphite in the stagnation pressure range 0.035 to 15 atmospheres (National Aeronautics and Space Administration ;, 1970), also by Howard G. Maahs (page images at HathiTrust)
• Langley Research Center: Ablative heat shield design for space shuttle (National Aeronautics and Space Administration ;, 1975), also by Rolf W. Seiferth and Martin Marietta Denver Aerospace (page images at HathiTrust)
• Langley Research Center: Ablative performance of uncoated silicone-modified and shuttle baseline reinforced carbon composites (National Aeronautics and Space Administration ;, 1976), also by Dennis L. Dicus, Ronald D. Brown, Russell N. Hopko, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Abnormal fault-recovery characteristics of the fault-tolerant multiprocessor uncovered using a new fault-injection methodology (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Peter A. Padilla (page images at HathiTrust)
• Langley Research Center: Abort performance for a winged-body single-stage to orbit vehicle (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by Jeffrey A. Lyon and Joint Institute for Advancement of Flight Sciences (page images at HathiTrust)
• Langley Research Center: Abort separation study of a shuttle orbiter and external tank at hypersonic speeds (National Aeronautics and Space Administration ;, 1975), also by Peter T. Bernot (page images at HathiTrust)
• Langley Research Center: Absolute calibration of a hydrogen discharge lamp in the vacuum ultraviolet (National Aeronautics and Space Administration ;, 1975), also by John E. Nealy (page images at HathiTrust)
• Langley Research Center: Absolute calibration of the RADSCAT scatterometer using precision spheres (National Aeronautics and Space Administration ;, 1976), also by William L. Grantham, John L. Mitchell, Lyle C. Schroeder, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Absorbed dose thresholds and absorbed dose rate limitations for studies of electron radiation effects on polyetherimides (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Edward R. Long (page images at HathiTrust)
• Langley Research Center: Acceleration of fatigue tests for built-up titanium components (U.S. National Aeronautics and Space Administration ;, 1976), also by R. T. Watanabe, United States National Aeronautics and Space Administration, and Boeing Company (page images at HathiTrust)
• Langley Research Center: Acceptability of VTOL aircraft noise determined by absolute subjective testing (National Aeronautics and Space Administration ;, 1972), also by Harry Sternfeld and Boeing Company (page images at HathiTrust)
• Langley Research Center: Accuracy and speed in computing the Chebyshev collocation derivative (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Wai Sun Don, Alex Solomonoff, and Brown University. Division of Applied Mathematics (page images at HathiTrust)
• Langley Research Center: Accuracy of aircraft velocities obtained from inertial navigation systems for application to airborne wind measurements (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Richard H. Rhyne and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Accuracy of finite element approximations to structural problems (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), also by Joseph E. Walz (page images at HathiTrust)
• Langley Research Center: Acoustic facilities for human factors research at NASA Langley Research Center : description and operational facilities (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Harvey H. Hubbard, Clemans A. Powell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Acoustic receptivity of compressible boundary layers : receptivity via surface-temperature variations (National Aeronautics and Space Administration, Langley Research Center ;, 1994), also by Meelan Choudhari (page images at HathiTrust)
• Langley Research Center: Acoustic theory of axisymmetric multisectioned ducts (National Aeronautics and Space Administration ;, 1974), also by W. E. Zorumski (page images at HathiTrust)
• Langley Research Center: Acoustic treatment of the NASA Langley 4- by 7-meter tunnel : a feasibility study (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by James C. Yu and A. Louis Abrahamson (page images at HathiTrust)
• Langley Research Center: Active Control for the Total-In-Flight Simulator (ACTIFS) (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by E. G. Rynaski, N. Weingarten, D. Andrisanti, Calspan Corporation, United States. Air Force. Systems Command, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Actively cooled plate fin sandwich structural panels for hypersonic aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by L. M. Smith, C. S. Beuyukian, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An actuator extension transformation for a motion simulator and an inverse transformation applying Newton-Raphson's method (National Aeronautics and Space Administration :, 1972), also by James E. Dieudonne, Richard E. Bardusch, Russell V. Parrish, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: ADAM, an axisymmetric duct aeroacoustic modeling system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by A. Louis Abrahamson, COMTEK (Firm), and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Adaptation of a general circulation model to ocean dynamics (National Aeronautics and Space Administration ;, 1976), also by Richard E. Turner, Gerard E. Woodbury, Thomas H. Rees, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Adaptation of the Theodorsen theory to the representation of an airfoil as a combination of a lifting line and a thickness distribution (National Aeronautics and Space Administration ;, 1975), also by Raymond L. Barger (page images at HathiTrust)
• Langley Research Center: Adaptive identification and control of structural dynamics using recursive lattice filters (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by N. Sundararajan, Jeffrey P. Williams, Raymond C. Montgomery, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Adaptive wall technology for minimization of wall interferences in transonic wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Stephen W. D. Wolf (page images at HathiTrust)
• Langley Research Center: Adaptive wall wind tunnels : a selected, annotated bibliography (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Marie H. Tuttle and Raymond E. Mineck (page images at HathiTrust)
• Langley Research Center: The admittance of a parallel-plate aperture illuminating a displaced dielectric-dielectric boundary (National Aeronautics and Space Administration ;, 1969), also by J. Earl Jones and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Advanced beaded and tubular structural panels (National Aeronautics and Space Administration ;, 1975), also by Max D. Musgrove, Bruce E. Greene, and Boeing Aerospace Company (page images at HathiTrust)
• Langley Research Center: Advanced emergency openings for commercial aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Laurence J. Bement and Morry L. Schimmel (page images at HathiTrust)
• Langley Research Center: Advanced group support systems and facilities (National Aeronautics and Space Administration, Langley Research Center, 1999), also by John B. Malone, Ahmed Khairy Noor, United States National Aeronautics and Space Administration, and University of Virginia. Center for Advanced Computational Technology (page images at HathiTrust; US access only)
• Langley Research Center: Advanced materials technology : proceedings of a seminar sponsored by NASA Langley Research Center, Hampton, Virginia, and the American Institute of Aeronautics and Astronautics, New York, and held in Hampton, Virginia, November 16-17, 1982 (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982), also by Louis A. Teichman, Charles P. Blankenship, American Institute of Aeronautics and Astronautics, and Va.) NASA/AIAA Advanced Materials Technology Seminar (1982 : Hampton (page images at HathiTrust)
• Langley Research Center: Advanced methods for calculating radiation transport in ablation-product contaminated boundary layers (National Aeronautics and Space Administration ;, 1970), also by William E. Nicolet and Aerotherm Corporation (page images at HathiTrust)
• Langley Research Center: Advanced missile technology : a review of technology improvement areas for cruise missiles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by L. L. Cronvich, H. P. Liepman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Advanced research : key to the future (For sale by the Superintendent of Documents, U. S. Govt. Print. Off, 1964) (page images at HathiTrust)
• Langley Research Center: Advanced stability theory analyses for laminar flow control (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Steven A. Orszag and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Advanced technology needs for a global change science program : perspective of the Langley Research Center (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Lawrence F. Rowell and Thomas J. Swissler (page images at HathiTrust)
• Langley Research Center: Advancements in structural dynamic technology resulting from Saturn 5 programs (National Aeronautics and Space Administration ;, 1970), also by P. J. Grimes and Boeing Company (page images at HathiTrust)
• Langley Research Center: Advances in contact algorithms and their application to tires (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Ahmed Khairy Noor and John A. Tanner (page images at HathiTrust)
• Langley Research Center: Advances in sterilization and decontamination : a survey submitted to National Aeronautics and Space Administration, Langley Research Center, Hampton, Virginia (Technology Utilization Office, National Aeronautics and Space Administration ;, 1978), also by Bionetics Corporation (page images at HathiTrust)
• Langley Research Center: Advancing-side directivity and retreating-side interactions of model rotor blade-vortex interaction noise (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by R. M. Martin (page images at HathiTrust)
• Langley Research Center: Aeordynamic characteristics of a distinct wing-body configuration at Mach 6 : experiment, theory, and the hypersonic isolation principle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Jim A. Penland and Jimmy L. Pittman (page images at HathiTrust)
• Langley Research Center: Aeorelastic analysis for helicopter rotor blades with time-variable, nonlinear structural twist and multiple structural redundancy-mathematical derivation and program user's manual (National Aeronautics and Space Administration ;, 1976), also by Richard L. Bielawa, United Technologies Research Center, United States National Aeronautics and Space Administration, and U.S. Army Air Mobility Research and Development Laboratory (page images at HathiTrust)
• Langley Research Center: Aeroacoustic data for high Reynolds number supersonic axisymmetric jets (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by John M. Seiner and Michael K. Ponton (page images at HathiTrust)
• Langley Research Center: Aeroacoustic research facilities at NASA Langley Research Center : description and operational characteristics (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Harvey H. Hubbard, James C. Manning, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Aeroacoustic wind-tunnel tests of a light twin-boom general aviation airplane with free or shrouded-pusher propellers (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by H. Clyde McLemore, Robert J. Pegg, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Aeroacoustics of flight vehicles : theory and practice (NASA Office of Management, Scientific and Technical Information Program, 1991), also by Harvey H. Hubbard, United States. Air Force. Wright Research and Development Center, and United States. Army Aviation Systems Command (page images at HathiTrust)
• Langley Research Center: Aerobrake concepts for NTP systems study (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Manuel I. Cruz and TRW Inc. Space and Technology Group (page images at HathiTrust)
• Langley Research Center: Aerodynamic analyses requiring advanced computers : a conference held at Langley Research Center in Hampton, Virginia on March 4-6, 1975 (National Aeronautics and Space Administration, Scientific and Technical Office ;, 1975) (page images at HathiTrust)
• Langley Research Center: Aerodynamic and acoustic tests of duct-burning turbofan exhaust nozzles (National Aeronautics and Space Administration ;, 1976), also by Hilary Kozlowski, Allan B. Packman, and Pratt & Whitney Aircraft Company (page images at HathiTrust)
• Langley Research Center: Aerodynamic and flow-visualization studies of variations in the geometry of irregular planform wings at a Mach number of 20.3 (National Aeronautics and Space Administration ;, 1974), also by David R. Stone and Bernard Spencer (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics at low Reynolds numbers of several heat-exchanger configurations for wind-tunnel use (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by William G. Johnson, William B. Igoe, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics at Mach 6 of a hypersonic research airplane concept having a 70 ̊swept delta wing (National Aeronautics and Space Administration ;, 1977), also by Louis E. Clark, Christine B. Richie, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics at Mach 6 of a wing-body concept for a hypersonic research airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by James L. Dillon, Jimmy L. Pittman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by A. Warner Robins, David S. Miller, Milton Lamb, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75 degree (National Aeronautics and Space Administration, 1960), also by Gerald V. Foster, Odell A. Morris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics in pitch of a 1/7-scale model of a two- and three-stage rocket configuration at Mach numbers of 0.4 to 4.63 (National Aeronautics and Space Administration ;, 1969), also by William F. Hinson, Roger H. Fournier, Richard A. Langhans, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of 0.187-scale model of a target missile at Mach 1.80 to 2.16 (National Aeronautics and Space Administration ;, 1966), also by William A. Corlett (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a 0.0667-scale model of the X-15A-2 research airplane at transonic speeds (National Aeronautics and Space Administration ;, 1966), also by James C. Patterson (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed (U.S. National Aeronautics and Space Administration ;, 1976), also by Raymond E. Mineck, James L. Hassell, Carl E. Freeman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a 55⁰ swept parawing with large-diameter leading edges (NASA :, 1964), also by Delwin R. Croom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a 60 degree sweptback-wing airplane configuration having tail surfaces located outboard of the wingtips at mach numbers of 2.30, 2.97, 3.51, and 4.06 (National Aeronautics and Space Administration, 1960), also by Jr. Sleeman, Roger H. Fournier, and James D. Church (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a five-jet VTOL configuration in the transition speed range (National Aeronautics and Space Administration ;, 1968), also by Richard J. Margason, Garl L. Gentry, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a fixed arrow-wing supersonic cruise aircraft at Mach numbers of 2.30, 2.70, and 2.95 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Odell A. Morris, Crolyn B. Watson, Dennis E. Fuller, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a hypersonic cruise aircraft concept with wing-mounted propulsion systems at mach numbers of 2.96, 3.96, and 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Gregory D. Riebe, Jimmy L. Pittman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Jim A. Penland, James B. Hallissy, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach number 0.2 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Jim A. Penland, James L. Dillon, Theodore R. Creel, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a large aircraft to transport space shuttle orbiter or other external payloads (National Aeronautics and Space Administration ;, 1975), also by John W. Paulson (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a parasol-wing--body combination utilizing favorable lift interference at Mach numbers from 3.00 to 4.63 (National Aeronautics and Space Administration ;, 1968), also by Odell A. Morris, Robert J. Mack, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a powered, externally blown flap STOL transport model with two engine simulator sizes (National Aeronautics and Space Administration ;, 1975), also by William G. Johnson (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a powered semispan tilting-shrouded-propeller VTOL model in hovering and transition flight (National Aeronautics and Space Administration, 1962), also by Kenneth W. Goodson, Kalman J. Grunwald, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a supersonic cruise airplane configuration at Mach numbers of 2.30, 2.96, and 3.30 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Barrett L. Shrout, Roger H. Fournier, and United States. National Aeronautics and Space Administration. Scientific and Technical Informaton Office (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Francis J. Capone, Dorothy Arbiter, and E. Ann Bare (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a swept-wing cruise missile at Mach numbers from 0.50 to 2.86 (National Aeronautics and Space Administration ;, 1972), also by M. Leroy Spearman and Ida K. Collins (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a tailless fixed-wing supersonic transport configuration at Mach number 2.20 (National Aeronautics and Space Administration, 1964), also by Gerald V. Foster and William A. Corlett (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing (National Aeronautics and Space Administration, 1964), also by Odell A. Morris and Dennis E. Fuller (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of a vectored-thrust V/STOL fighter in the transition-speed range (National Aeronautics and Space Administration ;, 1973), also by Raymond E. Mineck and Myles F. Schwendemann (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of forebody and nose strakes based on F-16 wind tunnel test experience ; prepared for Langley Research Center under contract NAS1-15006. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by H. W. Mann, J. N. Ralston, C. W. Smith, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of parawings having equal-length leading edges and keel (NASA, 1963), also by Rodger L. Naeseth, Thomas G. Gainer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of several current helicopter tail boom cross sections including the effect of spoilers (National Aeronautics and Space Administration, 1986), also by John C. Wilson, Henry L. Kelley, United States. Army Aviation Research and Technology Activity. Aerostructures Directorate, United States. Army Aviation Systems Command, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of three slender sharp-edge 74 ̊swept wings at subsonic, transonic, and supersonic Mach numbers (National Aeronautics and Space Administration ;, 1974), also by Edwin E. Davenport (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted V-tail (National Aeronautics and Space Administration, 1968), also by Richard J. Margason, Garl L. Gentry, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of vehicle bodies at crosswind conditions in ground proximity (National Aeronautics and Space Administration, 1970), also by Kalman J. Grunwald and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of wheelchairs (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Paul L. Coe and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Robert J. Mack (page images at HathiTrust)
• Langley Research Center: Aerodynamic characteristics, temperature, and noise measurements of a large-scale external-flow jet-augmented-flap model with turbojet engines operating (National Aeronautics and Space Administration, 1961), also by Marvin P. Fink and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic damping and oscillatory stability in pitch and yaw of Gemini configurations at Mach numbers from 0.50 to 4.63 (National Aeronautics and Space Administration ;, 1966), also by Bruce R. Wright and Robert A. Kilgore (page images at HathiTrust)
• Langley Research Center: Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by the free-oscillation method (National Aeronautics and Space Administration, 1960), also by W. J. Tuovila and R. W. Hess (page images at HathiTrust)
• Langley Research Center: Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap, and single propeller 0.22 chord below wing (National Aeronautics and Space Administration ;, 1969), also by Marvin P. Fink and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic design and analysis system for supersonic aircraft (National Aeronautics and Space Administration ;, 1975), also by W. D. Middleton, R. G. Coleman, J. L. Lundry, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Aerodynamic effects of bulbous bases (National Aeronautics and Space Administration ;, 1969), also by Lars E. Ericsson, J. Peter Reding, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Langley Research Center: Aerodynamic effects of five lift-fan pod arrangements on an unpowered V/STOL transport model (National Aeronautics and Space Administration ;, 1973), also by James L. Thomas, Delwin R. Croom, and Danny R. Hoad (page images at HathiTrust)
• Langley Research Center: Aerodynamic effects of some configuration variables on the aeroelastic characteristics of lifting surfaces at Mach numbers from 0.7 to 6.86 (National Aeronautics and Space Administration, 1961), also by Perry W. Hanson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic heating and loading within large open cavities in cone and cone-cyclinder-flare models at Mach 6.7 (National Aeronautics and Space Administration ;, 1974), also by L. Roane Hunt (page images at HathiTrust)
• Langley Research Center: Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 (National Aeronautics and Space Administration, 1960), also by Charles B. Rumsey, Russell N. Hopko, and Robert Owens Piland (page images at HathiTrust)
• Langley Research Center: Aerodynamic heating in large cavities in an array of RSI [reusable surface insulation] tiles (National Aeronautics and Space Administration ;, 1977), also by L. Roane Hunt and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic heating on the corrugated surface of a 10.2⁰ half-angle blunted cone at Mach 6.7 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Irving Weinstein, L. Roane Hunt, Don E. Avery, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Aerodynamic heating tests of missile stabilizers in a free jet at Mach number 2 (National Aeronautics and Space Administration, 1960), also by Louis F. Vosteen (page images at HathiTrust)
• Langley Research Center: Aerodynamic heating to the gaps and surfaces of simulated reusable-surface-insulation tile arrays in turbulent flow at Mach 6.6 (National Aeronautics and Space Administration ;, 1975), also by Irving Weinstein, Andrew J. Chapman, and Don E. Avery (page images at HathiTrust)
• Langley Research Center: Aerodynamic loading characteristics at Mach numbers from 0.80 to 1.20 of a 1/10-scale three-stage scout model (National Aeronautics and Space Administration, 1961), also by Thomas C. Kelly and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerodynamic loading characteristics of a 1/10-scale model of the three-stage Scout vehicle at Mach numbers 1.57 to 4.65 (National Aeronautics and Space Administration, 1963), also by Lloyd S. Jernell (page images at HathiTrust)
• Langley Research Center: Aerodynamic parameter estimation via Fourier modulating function techniques (National Aeronautics and Space Administration, Langley Research Center, 1995), also by A. E. Pearson (page images at HathiTrust)
• Langley Research Center: Aerodynamic pressure and heating-rate distributions in tile gaps around chine regions with pressure at a Mach number of 6.6 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by L. Roane Hunt and Kristopher K. Notestine (page images at HathiTrust)
• Langley Research Center: Aerodynamic roll damping of a T-tail transport configuration (National Aeronautics and Space Administration ;, 1974), also by Richmond P. Boyden (page images at HathiTrust)
• Langley Research Center: Aerodynamic testing technique for twin-fuselage models at hypersonic speeds (National Aeronautics and Space Administration ;, 1975), also by George C. Ashby (page images at HathiTrust)
• Langley Research Center: Aerodynamic tests and analysis of a turbojet-boosted launch vehicleconcept (spacejet) over a Mach number range of 1.50 to 2.86 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Gregory D. Riebe, Odell A. Morris, William J. Small, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Aeroelastic addition to NASTRAN (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by William P. Rodden, E. Dean Bellinger, and Robert L. Harder (page images at HathiTrust)
• Langley Research Center: Aeroelastic loads prediction for an arrow wing (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983), also by Christopher J. Borland and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by K. A. Yuan, Peretz Friedmann, and Los Angeles. Mechanical University of California (page images at HathiTrust)
• Langley Research Center: Aerofoil testing in a self-streamlining flexible walled wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Mark Charles Lewis (page images at HathiTrust)
• Langley Research Center: Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Francis J. Capone and Mary L. Mason (page images at HathiTrust)
• Langley Research Center: Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by George T. Carson and Milton Lamb (page images at HathiTrust)
• Langley Research Center: Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Francis J. Capone and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Aerothermal analysis of a wing-elevon cove with variable leakage (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by L. Roane Hunt and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Aerothermal and structural performance of a cobalt-base superalloy thermal protection system at Mach 6.6 (National Aeronautics and Space Administration ;, 1977), also by James Wayne Sawyer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Aerothermal environment in chordwise gaps between split elevons at Mach 6.8 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by L. Roane Hunt and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Aerothermal evaluation of a spherically blunted body with a trapezoidal cross section in the Langley 8-foot high-temperature tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Cindy W. Albertson (page images at HathiTrust)
• Langley Research Center: Aerothermal performance and structural integrity of a René 41 thermal protection system at Mach 6.6 (National Aeronautics and Space Administration ;, 1975), also by William D. Deveikis (page images at HathiTrust)
• Langley Research Center: Aerothermal tests of a 12.5⁰ cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Robert J. Nowak, L. Roane Hunt, and Cindy W. Albertson (page images at HathiTrust)
• Langley Research Center: Aerothermal tests of a heat-pipe-cooled leading edge at March 7 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Charles J. Camarda and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Aerothermal tests of quilted dome models on a flat plate at a Mach number of 6.5 (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Christopher E. Glass and L. Roane Hunt (page images at HathiTrust)
• Langley Research Center: Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Christopher E. Glass and L. Roane Hunt (page images at HathiTrust)
• Langley Research Center: Afterbody pressures on 2-dimensional boattailed bodies having turbulent boundary layers at Mach 5.98 (National Aeronautics and Space Administration :, 1964), also by W. Frank Staylor, Theodore J. Goldberg, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: Agricultural airplane mission time structure characteristics (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), also by Joseph W. Jewel and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Agricultural aviation research : a workshop (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1977), also by Louis F. Bouse, Howard L. Chevalier, and Texas A & M University (page images at HathiTrust)
• Langley Research Center: Aileron roll hysteresis effects on entry of space shuttle orbiter (National Aeronautics and Space Administration ;, 1977), also by Richard W. Powell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The air we breathe (National Aeronautics and Space Administration, Langley Research Center, in the 2000s), also by Irene Ladd and Wade Mickley (page images at HathiTrust)
• Langley Research Center: Airborne ballistic camera tracking systems (National Aeronautics and Space Administration ;, 1976), also by William L. Redish and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Airborne four-dimensional flight management in a time-based air traffic control environment (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by David H. Williams and Steven M. Green (page images at HathiTrust)
• Langley Research Center: Aircraft design for mission performance using nonlinear multiobjective optimization methods (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division :, 1990), also by Augustine R. Dovi and Gregory A. Wrenn (page images at HathiTrust)
• Langley Research Center: Aircraft emission inventories projected in year 2015 for a high speed civil transport (HSCT) universal airline network (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by Steven L. Baughcum, Stephen C. Henderson, and Boeing Company. Commercial Airplane Group (page images at HathiTrust)
• Langley Research Center: Aircraft noise prediction program user's manual (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Ronnie E. Gillian and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Aircraft propeller induced structure-borne noise (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by James F. Unruh and Southwest Research Institute (page images at HathiTrust)
• Langley Research Center: Aircraft tire behavior during high-speed operations in soil (National Aeronautics and Space Administration ;, 1972), also by Trafford J. W. Leland and Eunice G. Smith (page images at HathiTrust)
• Langley Research Center: Aircraft vortex wakes in relation to terminal operations (National Aeronautics and Space Administration, 1963), also by Joseph W. Wetmore, John P. Reeder, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: Airframe noise component interaction studies (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Martin R. Fink, Robert H. Schlinker, United Technologies Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Airframe noise of a small model transport aircraft and scaling effects (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John G. Shearin and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Airline pilot scan patterns during simulated ILS approaches (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Amos A. Spady (page images at HathiTrust)
• Langley Research Center: Airline transport pilot preferences for predictive informtion (National Aeronautics and Space Administration, Langley Research Center ;, 1996), also by Anna C. Trujillo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Airplane stability calculations with a card programmable pocket calculator (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Windsor L. Sherman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Airport-area airspace used in simulated operations with an experimental powered-lift STOL airplane (National Aeronautics and Space Administration ;, 1973), also by Norman S. Silsby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Airport noise impact reduction through operations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Richard DeLoach and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: AlGaAs single-mode stability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by D. Botez, I. Ladany, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and RCA Laboratories (page images at HathiTrust)
• Langley Research Center: Algebraic, geometric, and stochastic aspects of genetic operators (National Aeronautics and Space Administration ;, 1972), also by N. Y. Foo, Jack Bosworth, and University of Michigan (page images at HathiTrust)
• Langley Research Center: An algorithm for a general class of routine problems derived from Huygens' principle (National Aeronautics and Space Administration ;, 1974), also by Lee M. Avis and George R. Young (page images at HathiTrust)
• Langley Research Center: An algorithm for minimum-cost set-point ordering in a cryogenic wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John S. Tripp and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An algorithm for the weighting matrices in the sample-data optimal linear regulator problem (National Aeronautics and Space Administration ;, 1976), also by Ernest S. Armstrong, Alper K. Caglayan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Alternate multiple-outer-planet missions using a Saturn-Jupiter flyby sequence (National Aeronautics and Space Administration ;, 1973), also by John W. Young and Margery E. Hannah (page images at HathiTrust)
• Langley Research Center: An alternating direction implicit method for the control data STAR-100 vector computer (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Jules J. Lambiotte and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Ambient temperature fatigue tests of elements of an actively cooled honeycomb sandwich structural panel (National Aeronautics and Space Administration ;, 1977), also by Ellsworth L. Sharpe, Wolf Elber, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Amplified crossflow disturbances in the laminar boundary layer on swept wings with suction (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by J. Ray Dagenhart and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Analog-digital simulation of transient-induced logic errors and upset susceptibility of an advanced control system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Victor A. Carreno, R. K. Iyer, and G. Choi (page images at HathiTrust)
• Langley Research Center: An analog study of an airborne automatic landing-approach system (National Aeronautics and Space Administration, 1959), also by James J. Adams (page images at HathiTrust)
• Langley Research Center: Analog techniques for measuring the frequency response of linear physical systems excited by frequency-sweep inputs (National Aeronautics and Space Administration :, 1960), also by Wilmer H. Reed, Lawrence E. Barker, and Albert W. Hall (page images at HathiTrust)
• Langley Research Center: Analysis and compilation of missile aerodynamic data. (National Aeronautics and Space Administration ;, 1977), also by James O. Nichols, Auburn University. Dept. of Aerospace Engineering, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analysis and compilation of missile aerodynamic data (National Aeronautics and Space Administration ;, 1977), also by John E. Burkhalter, Auburn University. Dept. of Aerospace Engineering, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analysis and development of dynamic selection of laser array elements (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by M. D. Williams (page images at HathiTrust)
• Langley Research Center: Analysis and preliminary design of an advanced technology transport flight control system (National Aeronautics and Space Administration ;, 1975), also by Ronald Frazzini, Darrel Vaughn, and Honeywell Inc. Government and Aeronautical Products Division (page images at HathiTrust)
• Langley Research Center: Analysis and testing of axial compression in imperfect slender truss struts (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Mark S. Lake and Nicholas Georgiadis (page images at HathiTrust)
• Langley Research Center: Analysis and testing of high entrainment single nozzle jet pumps with variable mixing tubes (National Aeronautics and Space Administration ;, 1972), also by Kenneth E. Hickman, Gerald B. Gilbert, Philip G. Hill, and Dynatech R/D Company (page images at HathiTrust)
• Langley Research Center: Analysis and testing of the SURE program (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Kelly J. Dotson (page images at HathiTrust)
• Langley Research Center: Analysis, design and test of acoustic treatment in a laboratory inlet duct (National Aeronautics and Space Administration ;, 1979), also by R. E. Kraft (page images at HathiTrust)
• Langley Research Center: An analysis method for two-dimensional transonic viscous flow (National Aeronautics and Space Administration ;, 1975), also by Paul C. Bavitz (page images at HathiTrust)
• Langley Research Center: An analysis of a charring ablator with thermal nonequilibrium, chemical kinetics, and mass transfer (National Aeronautics and Space Administration ;, 1973), also by Ronald K. Clark (page images at HathiTrust)
• Langley Research Center: Analysis of a linear system for variable-thrust control in the terminal phase of rendezvous (National Aeronautics and Space Administration, 1961), also by Richard A. Hord, Barbara J. Durling, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analysis of a turbulent boundary layer over a moving ground plane (National Aeronautics and Space Administration ;, 1972), also by Alan T. Roper and Garl L. Gentry (page images at HathiTrust)
• Langley Research Center: Analysis of acceleration, airspeed and gust-velocity data from a four-engine turboprop transport operating over the eastern United States (National Aeronautics and Space Administration, 1959), also by Martin R. Copp and Mary W. Fetner (page images at HathiTrust)
• Langley Research Center: Analysis of an existing experiment on the interaction of acoustic waves with a laminar boundary layer (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by M. R. Schopper, Systems and Applied Sciences Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Analysis of bonded joints (National Aeronautics and Space Administration ;, 1975), also by S. Srinivas (page images at HathiTrust)
• Langley Research Center: An analysis of combustion studies in shock expansion tunnels and reflected shock tunnels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Casimir J. Jachimowski (page images at HathiTrust)
• Langley Research Center: Analysis of dynamic stall using unsteady boundary-layer theory (National Aeronautics and Space Administration ;, 1974), also by R. M. Scruggs, R. E. Singleton, John F. Nash, and Inc Scientific & Business Consultants (page images at HathiTrust)
• Langley Research Center: Analysis of effects of interceptor roll performance and maneuverability on success of collision-course attack (National Aeronautical and Space Administration, 1961), also by William H. Phillips and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analysis of experimental results of the inlet for the NASA hypersonic research engine aerothermodynamic integration model (U.S. National Aeronautics and Space Administration ;, 1976), also by Earl H. Andrews, Ernest A. Mackley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analysis of finite-size phased arrays of circular waveguide elements (National Aeronautics and Space Administration, 1974), also by M. C. Bailey and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analysis of flight data from a high-incidence research model by system identification methods (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by James G. Batterson and Vladislav Klein (page images at HathiTrust)
• Langley Research Center: Analysis of flight data on boundary layer transition at high angles of attack (National Aeronautics and Space Administration ;, 1972), also by Wayne W. Haigh, D. R. S. Ko, B. M. Lake, and TRW Systems Group (page images at HathiTrust)
• Langley Research Center: An analysis of flight test data on the C-141A aircraft (National Aeronautics and Space Administration ;, 1970), also by J. H. Paterson and Lockheed-Georgia Company (page images at HathiTrust)
• Langley Research Center: Analysis of general aviation single-pilot IFR incident data obtained from the NASA Aviation Safety Reporting System (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Hugh P. Bergeron (page images at HathiTrust)
• Langley Research Center: Analysis of graphite/polyimide rail shear specimens subjected to mechnaical and thermal loading (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Terry A. Weisshaar, Ramon Garcia, Virginia Polytechnic Institute and State University, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Analysis of helicopter maneuver-loads and rotor-loads flight-test data (National Aeronautics and Space Administration ;, 1973), also by Edward A. Beno and United Aircraft Corporation. Sikorsky Aircraft Division (page images at HathiTrust)
• Langley Research Center: Analysis of helicopter rotor blade torsional oscillations due to stall (National Aeronautics and Space Administration ;, 1975), also by Peter Crimi, U.S. Army Air Mobility Research and Development Laboratory, and Avco Corporation. Systems Division (page images at HathiTrust)
• Langley Research Center: Analysis of high-aspect-ratio jet-flap wings of arbitrary geometry (National Aeronautics and Space Administration ;, 1973), also by Peter B. S. Lissaman and Northrop Corporate Laboratories (page images at HathiTrust)
• Langley Research Center: Analysis of human response in combined control tasks (National Aeronautics and Space Administration ;, 1968), also by Hugh P. Bergeron, George J. Hurt, and James J. Adams (page images at HathiTrust)
• Langley Research Center: Analysis of hypersonic pressure and heat transfer tests on a flat plate with a flap and a delta wing with body, elevons, fins, and rudders (National Aeronautics and Space Administration :, 1966), also by H. L. Giles and J. W. Thomas (page images at HathiTrust)
• Langley Research Center: Analysis of hypersonic pressure and heat transfer tests on delta wings with laminar and turbulent boundary layers (National Aeronautics and Space Administration, 1966), also by A. L. Nagel, L. B. Doyle, and H. D. Fitzsimmons (page images at HathiTrust)
• Langley Research Center: An analysis of incremental horizontal-tail loads measured on a swept-wing bomber airplane in sideslip maneuvers (National Aeronautics and Space Administration, 1959), also by William A. McGowan (page images at HathiTrust)
• Langley Research Center: Analysis of laminated, composite, circular cylindrical shells with general boundary conditions (National Aeronautics and Space Administration, 1974), also by S. Srinivas (page images at HathiTrust)
• Langley Research Center: Analysis of limited memory estimators and their application to spacecraft attitude determination (National Aeronautics and Space Administration ;, 1970), also by Edwin C. Foudriat and Marquette University (page images at HathiTrust)
• Langley Research Center: Analysis of materials flown on the Long Duration Exposure Facility : summary of results of the Materials Special Investigation Group (National Aeronautics and Space Administration, Langley Research Center, 1995), also by H. Gary Pippin (page images at HathiTrust)
• Langley Research Center: Analysis of maximum range trajectories for rocket-propelled lunar flying vehicles in a uniform gravitational field (National Aeronautics and Space Administration ;, 1969), also by A. Gary Childs, Ernest S. Armstrong, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analysis of objects in binary images (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Desiree M. Leonard and Computer Sciences Corporation (page images at HathiTrust)
• Langley Research Center: Analysis of oscillatory motion of a light airplane at high values of lift coefficient (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by James G. Batterson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Analysis of oscillatory pressure data including dynamic stall effects (National Aeronautics and Space Administration ;, 1974), also by F. O. Carta and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
• Langley Research Center: Analysis of preflutter and postflutter charactristics with motion-matched aerodynamic forces (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Herbert J. Cunningham and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Analysis of rotary balance data for the F-15 airplane including the effect of conformal fuel tanks (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Billy Barnhart and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Analysis of selected materials flown on interior locations of the long duration exposure facility (National Aeronautics and Space Administration, Langley Research Center, 1994), also by H. A. Smith (page images at HathiTrust)
• Langley Research Center: An analysis of shock coalescence including three-dimensional effects with application to sonic boom extrapolation (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), also by Christine M. Darden and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Analysis of silverized teflon thermal control material flown on the Long Duration Exposure Facility (National Aeronautics and Space Administration, Langley Research Center, 1995), also by H. Gary Pippin (page images at HathiTrust)
• Langley Research Center: Analysis of six broadband optical filters for measuring chlorophyll a and suspended solids in the Patuxent River (U.S. National Aeronautics and Space Administration ;, 1976), also by Craig W. Ohlhorst and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analysis of sonic boom measurements near shock wave extremities for flight near Mach 1.0 and for airplane accelerations (National Aeronautics and Space Administration ;, 1974), also by George T. Haglund, Edward J. Kane, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Analysis of stability contributions of high dihedral V-trails (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Carl F. Freeman, William T. Yeager, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Analysis of stall flutter of a helicopter rotor blade (National Aeronautics and Space Administration ;, 1973), also by Peter Crimi and Avco Corporation. Systems Division (page images at HathiTrust)
• Langley Research Center: An analysis of terrain bias error in planetary radar altimeters (National Aeronautics and Space Administration ;, 1969), also by Richard F. Harrington, William D. Stanley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An analysis of the crossover between local and massive separation on airfoils (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by M. Burnett and J. E. Carter (page images at HathiTrust)
• Langley Research Center: Analysis of the dynamic lateral stability of a delta-wing airplane with frequency-dependent stability derivatives (National Aeronautics and Space Administration, 1959), also by Albert E. Brown and Albert A. Schy (page images at HathiTrust)
• Langley Research Center: An Analysis of the facsimile-camera response to radiant point sources (National Aeronautics and Space Administration ;, 1973), also by Friedrich O. Huck (page images at HathiTrust)
• Langley Research Center: Analysis of the feasibility of an experiment to measure carbon monoxide in the atmosphere (National Aeronautics and Space Administration ;, 1973), also by M. H. Bortner and General Electric Company (page images at HathiTrust)
• Langley Research Center: Analysis of the gamma-ray-backscatter technique for direct measurement of the density of the Martian atmosphere (National Aeronautics and Space Administration ;, 1969), also by Peter J. LeBel (page images at HathiTrust)
• Langley Research Center: Analysis of the injection of a heated turbulent jet into a cross flow (National Aeronautics and Space Administration, 1973), also by James F. Campbell and Joseph A. Schetz (page images at HathiTrust)
• Langley Research Center: An analysis of the operation of a mass measuring system in an orbiting spacecraft (National Aeronautics and Space Administration ;, 1969), also by Bruce A. Conway and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analysis of the performance of the drive system and diffuser of the Langley Unitary Plan Wind Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Lowell E. Hasel, Robert L. Stallings, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Analysis of the physical atomic forces between noble gas atoms, alkali ions, and halogen ions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by John W. Wilson, R. A. Outlaw, and John H. Heinbockel (page images at HathiTrust)
• Langley Research Center: An analysis of the relaxation of laminar boundary layer on a flat plate after passage of an interface with application to expansion-tube flows (National Aeronautics and Space Administration ;, 1972), also by Roop N. Gupta (page images at HathiTrust)
• Langley Research Center: Analysis of the scramjet inlet flow field using two-dimensional Navier-Stokes equations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), also by Ajay Kumar, S. N. Tiwari, Old Dominion University. Research Foundation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Analysis of the space shuttle orbiter entry dynamics from Mach 10 to Mach 2.5 with the November 1976 flight control system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Richard W. Powell and Howard W. Stone (page images at HathiTrust)
• Langley Research Center: Analysis of transonic flow about lifting wing-body configurations (National Aeronautics and Space Administration ;, 1975), also by Richard W. Barnwell (page images at HathiTrust)
• Langley Research Center: Analysis of validation tests of the Langley pilot transonic cryogenic tunnel (National Aeronautics and Space Administration ;, 1975), also by Edward J. Ray (page images at HathiTrust)
• Langley Research Center: Analysis of variable property turbulent boundary layers by means of a modified compressibility transformation (National Aeronautics and Space Administration ;, 1972), also by C. Economos, J. L. Boccio, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Langley Research Center: Analysis of various descent trajectories for a hypersonic-cruise, cold-wall research airplane (National Aeronautics and Space Administration ;, 1975), also by Pierce L. Lawing (page images at HathiTrust)
• Langley Research Center: Analysis of VGH data from two types of four-engine airplanes in commercial cargo service (National Aeronautics and Space Administration ;, 1972), also by Frederick M. Healy (page images at HathiTrust)
• Langley Research Center: Analysis of wing-body interaction flutter for a preliminary space shuttle design (National Aeronautics and Space Administration ;, 1974), also by Richard R. Chipman, Peter Shyprykevich, and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: An Analytic and experimental evaluation of flowing air test conditions for selected metallics in a shuttle TPS application (National Aeronautics and Space Administration ;, 1975), also by John W. Schaefer and Acurex Corporation. Aerotherm Division (page images at HathiTrust)
• Langley Research Center: Analytic model for washout of HCℓ(g) from dispersing rocket exhaust clouds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by G. L. Pellett and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Analytic studies of local-severe-storm observables by satellites (National Aeronautics and Space Administration ;, 1977), also by Paul Dergarabedian, Francis Fendell, and TRW Systems and Energy (page images at HathiTrust)
• Langley Research Center: Analytic studies of sound pressures inside the duct of ducted propellers (National Aeronautics and Space Administration :, 1971), also by Joseph A. Drischler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analytic studies on satellite detection of severe, two-cell tornadoes (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by George F. Carrier, Francis E. Fendell, Paul Dergarabedian, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Analytic study of induced pressure on long bodies of revolution with varying nose bluntness at hypersonic speeds (U.S. G.P.O., 1960), also by Vernon Van Hise and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analytical and design techniques for drag reduction studies on wavy surfaces (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by R. Balasubramanian and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Analytical and experimental investigation of aircraft metal structures reinforced with filamentary composites (National Aeronautics and Space Administration ;, 1971), also by S. Oken, Boeing Commercial Airplane Company, Boeing Company, and Boeing Company. Commercial Airplane Group (page images at HathiTrust)
• Langley Research Center: Analytical and experimental investigation of fatigue in a sheet specimen with an interference-fit bolt (National Aeronautics and Space Administration ;, 1975), also by John H. Crews (page images at HathiTrust)
• Langley Research Center: Analytical and experimental studies for predicting noise attenuation in acoustically treated ducts for turbofan engines (National Aeronautics and Space Administration ;, 1969), also by Ernest Feder, Lee Wallace Dean, and United Aircraft Corporation (page images at HathiTrust)
• Langley Research Center: Analytical and experimental studies of shock interference heating in hypersonic flows (National Aeronautics and Space Administration ;, 1973), also by J. Wayne Keyes, Frank D. Hains, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analytical and experimental study of the effects of wing-body aerodynamic interaction on space shuttle subsonic flutter (National Aeronautics and Space Administration ;, 1975), also by Richard R. Chipman, Frank J. Rauch, and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Analytical and experimental vibration studies of a 1/8 scale shuttle orbiter (National Aeronautics and Space Administration ;, 1975), also by Larry D. Pinson (page images at HathiTrust)
• Langley Research Center: Analytical and photogrammetric characterization of a planar tetrahedral truss (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by K. Chauncey Wu, Marvin D. Rhodes, and Richard R. Adams (page images at HathiTrust)
• Langley Research Center: Analytical and preliminary simulation study of a pilot's ability to control the terminal phase of a rendezvous with simple optical devices and a timer (National Aeronautics and Space Administration, 1961), also by Edgar C. Lineberry, Max C. Kurbjun, Roy F. Brissenden, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analytical and simulator study of advanced transport handling qualities (National Aeronauticas and Space Administration, Scientific and Technical Information Office ;, 1982), also by William H. Levison, William W. Rickard, Beranek Bolt, Douglas Aircraft Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Analytical chemical kinetic investigation of the effects of oxygen, hydrogen, and hydroxyl radicals on hydrogen-air combustion (National Aeronautics and Space Administration ;, 1974), also by George T. Carson (page images at HathiTrust)
• Langley Research Center: Analytical comparison of hypersonic flight and wind tunnel viscous/inviscid flow fields (National Aeronautics and Space Administration ;, 1975), also by H. J. Fivel, L. J. Mockapetris, R. V. Masek, and McDonnell Douglas Astronautics Company-East (page images at HathiTrust)
• Langley Research Center: An analytical evaluation of airfoil sections for helicopter rotor applications (National Aeronautics and Space Administration ;, 1975), also by Gene J. Bingham (page images at HathiTrust)
• Langley Research Center: Analytical evaluation of jet noise source location technique utilizing an acoustically hard baffle with aperture (National Aeronautics and Space Administration ;, 1973), also by Thomas D. Norum, Edward P. McDaid, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An analytical evaluation of the denting of airplane surfaces by hail / by Robert G. Thomson and Robert J. Hayduk. (National Aeronautics and Space Administration, 1969), also by Robert G. Thomson, Robert J. Hayduk, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: Analytical expressions for position error in triangulation solution of point in space for several station configurations (National Aeronautics and Space Administration ;, 1974), also by Sheila Ann T. Long (page images at HathiTrust)
• Langley Research Center: Analytical investigation and prediction of spin and recovery characteristics of the North American X-15 airplane (National Aeronautics and Space Administration, 1960), also by William D. Grantham and Stanley H. Scher (page images at HathiTrust)
• Langley Research Center: An analytical investigation of a simplified thrust-vector orientation technique for establishing lunar orbits (National Aeronautics and Space Administration ;, 1966), also by L. Keith Barker and Gene W. Sparrow (page images at HathiTrust)
• Langley Research Center: An analytical investigation of ablation (National Aeronautics and Space Administration, 1960), also by Bernard Rashis and Russell N. Hopko (page images at HathiTrust; US access only)
• Langley Research Center: Analytical investigation of effect of spin entry technique on spin and recovery characteristics for a 60 degree delta-wing airplane (National Aeronautics and Space Administration, 1959), also by Stanley H. Scher, George F. Lawrence, and Ernie L. Anglin (page images at HathiTrust)
• Langley Research Center: Analytical investigation of fan tone noise due to ingested atmospheric turbulence (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Ulrich W. Ganz and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Analytical investigation of synchrophasing as a means of reducing aircraft interior noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by C. R. Fuller, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Langley Research Center: Analytical investigation of the effects of blade flexibility, unsteady aerodynamics, and variable inflow on helicopter rotor stall characteristics (National Aeronautics and Space Administration, 1971), also by E. D. Bellnger, United States National Aeronautics and Space Administration, and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
• Langley Research Center: Analytical investigation of the landing dynamics of a large airplane with a load-control system in the main landing gear (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by John R. McGehee and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Analytical investigation of the motion of a clamshell-type heat shield on deployment from a parent vehicle in the atmosphere (National Aeronautics and Space Administration ;, 1966), also by Ross L. Goble (page images at HathiTrust)
• Langley Research Center: An analytical investigation of the performance of solar collectors as nighttime heat radiators in airconditioning cycles (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Clay B. Jones, Frederick O. Smetana, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Analytical investigations in aircraft and spacecraft trajectory optimization and optimal guidance (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by Nikos Markopoulos, Anthony J. Calise, and Georgia Institute of Technology. School of Aerospace Engineering (page images at HathiTrust)
• Langley Research Center: Analytical method for determining the stability of linear retarded sytems with two delays (National Aeronautics and Space Administration ;, 1975), also by L. Keith Barker and J. L. Whitesides (page images at HathiTrust)
• Langley Research Center: An analytical method for ditching analysis of an airborne vehicle (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Farhad Ghaffari (page images at HathiTrust)
• Langley Research Center: Analytical method for predicting the pressure distribution about a nacelle at transonic speeds (National Aeronautics and Space Administration ;, 1973), also by J. S. Keith and General Electric Company (page images at HathiTrust)
• Langley Research Center: Analytical modeling of the structureborne noise path on a small twin-engine aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by J. E. Cole (page images at HathiTrust)
• Langley Research Center: Analytical parametric investigation of low pressure ratio fan noise (National Aeronautics and Space Administration ;, 1973), also by F. B. Metzger and United Aircraft Corporation. Hamilton Standard Division (page images at HathiTrust)
• Langley Research Center: An Analytical procedure for computing smooth transitions between two specified cross sections with applications to blended wing-body configurations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Raymond L. Barger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An analytical procedure for optimizing television systems for planetary descent missions (National Aeronautics and Space Administration ;, 1969), also by Friedrich O. Huck and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analytical properties of noise generating mechanisms in a supersonic jet exhaust flow (National Aeronautics and Space Administration ;, 1971), also by S. Paul Pao and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analytical studies of separated vortex flow on highly swept wings (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by John M. Kuhlman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Analytical study of acoustic response of a semireverberant enclosure with application to active noise control (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Tony L. Parrott, Doreen Gridley, and David B. Schein (page images at HathiTrust)
• Langley Research Center: An analytical study of aircraft lateral-directional handling qualities using pilot models (National Aeronautics and Space Administration ;, 1976), also by James J. Adams and Frederick L. Moore (page images at HathiTrust)
• Langley Research Center: Analytical study of diffusion-controlled char oxidation and its effect on steady-state ablation of plastic materials (National Aeronautics and Space Administration, 1966), also by Gerald D. Walberg and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analytical study of effects of autopilot operation on motions of a subsonic jet-transport airplane in severe turbulence (National Aeronautics and Space Administration, 1970), also by Wiliam P. Gilbert and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analytical study of effects of severe turbulence on flight motions of a typical subsonic jet-transport airplane (National Aeronautics and Space Administration, 1969), also by William D. Grantham, Mary S. Adams, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An analytical study of hydrogen cooled panels for application to hypersonic aircraft (National Aeronautics and Space Administrtion, 1971), also by W. G. Flieder, Garrett Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Analytical study of rigidized fibrous materials (National Aeronautics and Space Administration ;, 1974), also by B. Walter Rosen, John J. Kibler, Debal Bagchi, and Materials Sciences Corporation (page images at HathiTrust)
• Langley Research Center: An analytical study of the effects of jets located more than one jet diameter above a wing at subsonic speeds (National Aeronautics and Space Administration ;, 1974), also by Lawrence E. Putnam (page images at HathiTrust)
• Langley Research Center: An analytical study of the hydrogen-air reaction mechanism with application to scramjet combustion (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Casimir J. Jachimowski (page images at HathiTrust)
• Langley Research Center: An analytical study of the longitudinal response of airplanes to positive wind shear (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Windsor L. Sherman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Analytical study of the performance of a gust alleviation system for a STOL airplane (National Aeronautics and Space Administration ;, 1973), also by Waldo I. Oehman (page images at HathiTrust)
• Langley Research Center: Analytical study of the performance of a gust alleviation system with a vane sensor (National Aeronautics and Space Administration ;, 1974), also by Waldo I. Oehman (page images at HathiTrust)
• Langley Research Center: An analytical study of the reponse of a constant-attitude aircraft to atmospheric turbulence (National Aeronautics and Space Administration ;, 1973), also by Frederick O. Smetana, Ronald K. Carden, and North Carolina State University (page images at HathiTrust)
• Langley Research Center: An analytical study of turbulence responses, including horizontal-tail loads, of a control-configured vehicle with relaxed static stability (U.S. National Aeronautics and Space Administration ;, 1976), also by Boyd Perry (page images at HathiTrust)
• Langley Research Center: An analytical technique for approximating unsteady aerodynamics in the time domain / H.J. Dunn. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by H. J. Dunn and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Analytical techniques of pilot scanning behavior and their application (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Randall L. Harris, Amos A. Spady, and Bobby J. Glover (page images at HathiTrust)
• Langley Research Center: Angle-of-attack analysis for Project Fire 1 payload reentry flight (National Aeronautics and Space Administration ;, 1966), also by Gerard E. Woodbury (page images at HathiTrust)
• Langley Research Center: Annealing of 22-, 40-, and 158-MeV proton damage in n- and p-type silicon (National Aeronautics and Space Administration ;, 1969), also by Marvin E. Beatty and Gerald Franklin Hill (page images at HathiTrust)
• Langley Research Center: Annealing of aromatic polyimide precursors (National Aeronautics and Space Administration ;, 1975), also by N. T. Wakelyn (page images at HathiTrust)
• Langley Research Center: Annoyance caused by advanced turboprop aircraft flyover noise : comparison of different propeller configurations (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by David A. McCurdy (page images at HathiTrust)
• Langley Research Center: Annoyance caused by advanced turboprop aircraft flyover noise : counter-rotating propeller configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by David A. McCurdy (page images at HathiTrust)
• Langley Research Center: Annoyance caused by propeller airplane flyover noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by David A. McCurdy and Clemans A. Powell (page images at HathiTrust)
• Langley Research Center: Annoyance due to multiple airplane noise exposure (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Clemans A. Powell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Annoyance response to simulated advanced turboprop aircraft interior noise containing tonal beats (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Jack D. Leatherwood (page images at HathiTrust)
• Langley Research Center: The annular momentum control device (AMCD) and potential applications (National Aeronautics and Space Administration ;, 1975), also by Willard W. Anderson and Nelson J. Groom (page images at HathiTrust)
• Langley Research Center: The annular suspension and pointing (ASP) system for space experiments and predicted point accuracies (National Aeronautics and Space Administration ;, 1975), also by Willard W. Anderson and S. M. Joshi (page images at HathiTrust)
• Langley Research Center: Aperture excited dielectric antennas (National Aeronautics and Space Administration ;, 1974), also by W. F. Croswell (page images at HathiTrust)
• Langley Research Center: Apollo Saturn 511 effluent measurements from the Apollo 16 launch operations : an experiment (National Aeronautics and Space Administration ;, 1974), also by Gerald L. Gregory, Dewey E. Wornom, and William C. Hulten (page images at HathiTrust)
• Langley Research Center: Apparatus description and data analysis of a radiometric technique for measurements of spectral and total normal emittance (National Aeronautics and Space Administration ;, 1975), also by S. Franklin Edwards (page images at HathiTrust)
• Langley Research Center: Applicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edges (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Harry W. Carlson and Christine M. Darden (page images at HathiTrust)
• Langley Research Center: Application of a 1-strip integral method to the unsteady supersonic aerodynamics of an inclined flat surface (National Aeronautics and Space Administration :, 1972), also by Robert M. Bennett and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An application of a linear programming technique to nonlinear minimax problems (National Aeronautics and Space Administration ;, 1973), also by James R. Schiess (page images at HathiTrust)
• Langley Research Center: Application of a numerical orthogonal coordinate generator to axisymmetric blunt bodies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Randolph A. Graves and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Application of a numerically generated orthogonal coordinate system to the solution of inviscid axisymmetric supersonic flow over blunt bodies (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by H. Harris Hamilton, Randolph A. Graves, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Application of a PC-based, real-time, data-acquisition system in rotorcraft wind-tunnel testing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Matthew L. Wilbur (page images at HathiTrust)
• Langley Research Center: Application of a supersonic kernel-function procedure to flutter analysis of thin lifting surfaces (National Aeronautics and Space Administration :, 1970), also by Herbert J. Cunningham and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The application of acoustic emission technique to fatigue crack measurement (National Aeronautics and Space Administration ;, 1974), also by Jag J. Singh, John H. Crews, and William T. Davis (page images at HathiTrust)
• Langley Research Center: Application of cell culture as a primary toxicity screen of possible spacecraft contaminants (National Aeronautics and Space Administration ;, 1967), also by Richard B. Hays (page images at HathiTrust)
• Langley Research Center: Application of Dorodnitsyn's integral method to nonequilibrium flows over pointed bodies (National Aeronautics and Space Administration, 1963), also by Jerry C. South (page images at HathiTrust)
• Langley Research Center: Application of higher harmonic blade feathering on the OH-6A helicopter for vibration reduction (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by F. K. Straub, E. V. Byrns, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and McDonnell Douglas Helicopter Company (page images at HathiTrust)
• Langley Research Center: Application of In Situ Fiberization for fabrication of improved strain isolation pads and graphite-epoxy composites (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by R. W. Rosser, D. I. Basiulis, R. W. Seibold, Hughes Aircraft Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Application of information theory to the design of line-scan imaging systems (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Friedrich O. Huck and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Application of LQG/LTR technique to robust controller synthesis for a large flexible space antenna (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by S. M. Joshi, N. Sundararajan, and Ernest S. Armstrong (page images at HathiTrust)
• Langley Research Center: Application of mathematical optimization procedures to a structural model of a large finite-element wing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Joanne L. Walsh (page images at HathiTrust)
• Langley Research Center: Application of maximum likelihood techniques to the design of optimum star trackers (National Aeronautics and Space Administration ;, 1968), also by Edwin C. Foudriat and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Application of model control to wing-flutter suppression (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Aaron J. Ostroff, Samuel Pines, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Application of modified profile analysis to function testing of simulated CTOL transport touchdown-performance data (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Russell V. Parrish, Burnell T. McKissick, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Application of modified profile analysis to function testing of the motion/no-motion issue in an aircraft ground-handling simulation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Russell V. Parrish, George G. Steinmetz, Burnell T. McKissick, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An application of multivariable design techniques to the control of the National Transonic Facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Ernest S. Armstrong, John S. Tripp, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Application of multivariable search techniques to structural design optimization (National Aeronautics and Space Administration ;, 1972), also by Robert T. Jones, D. S. Hague, and Aerophysics Research Corporation (page images at HathiTrust)
• Langley Research Center: Application of Newton's method to postbuckling of rings under pressure loadings (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Gaylen A. Thurston (page images at HathiTrust)
• Langley Research Center: Application of nonlinear adaptive motion washout to transport ground-handling simulation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Russell V. Parrish and Dennis J. Martin (page images at HathiTrust)
• Langley Research Center: Application of phase-change technique to thin sections with heating on both surfaces (National Aeronautics and Space Administration ;, 1973), also by James L. Hunt, Christine B. Richie, and Joan I. Pitts (page images at HathiTrust)
• Langley Research Center: Application of pressurized liquid nitrogen inside parametric-amplifier structures for input-noise-temperature improvement (National Aeronautics and Space Administration ;, 1969), also by Hans-Juergen C. Blume (page images at HathiTrust)
• Langley Research Center: Application of queueing models to multiprogrammed computer systems operating in a time-critical environment (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Dave E. Eckhardt and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An application of similitude to model design of a soil-projectile system (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), also by Katsuyuki Awoshika, William Roy Cox, and University of Texas (page images at HathiTrust; US access only)
• Langley Research Center: Application of sonic-boom minimization concepts in supersonic transport design (National Aeronautics and Space Administration ;, 1973), also by Harry W. Carlson, Robert J. Mack, and Raymond L. Barger (page images at HathiTrust)
• Langley Research Center: Application of supersonic linear theory and hypersonic impact methods to three nonslender hypersonic airplane concepts at mach numbers from 1.10 to 2.86 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Jimmy L. Pittman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Application of the aerodynamic energy concept to flutter suppression and gust alleviation by use of active controls (National Aeronautics and Space Administration ;, 1976), also by E. Nissim, A. Caspi, I. Lottati, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Application of the Hughes-Liu algorithm to the two-dimensional heat equation / David S. Malkus and Peter I. Reichmann, Raphael T. Haftka ; prepared for Langley Research Center under grant NAG1-224 and NSG-1266. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by David S. Malkus, Raphael T. Haftka, Peter I. Reichmann, Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept, Illinois Institute of Technology. Dept. of Mathematics, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An application of theory to axial compressor noise (National Aeronautics and Space Administration, 1970), also by J. B. Ollerhead, C. L. Munch, United States National Aeronautics and Space Administration, and Wyle Laboratories (page images at HathiTrust)
• Langley Research Center: Application of two design methods for active flutter suppression and wind-tunnel test results (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Jerry R. Newsom, H. J. Dunn, Irving Abel, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Elizabeth B. Plentovich (page images at HathiTrust)
• Langley Research Center: Applications of analytic function theory to analysis of single-sideband angle-modulated systems (National Aeronautics and Space Administration ;, 1969), also by John Hoyt Painter and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Applications of formal methods to specification and safety of avionics software (National Aeronautics and Space Administration, Langley Research Center ;, 1996), also by D. N. Hoover, Polar Humann, David Guaspari, and Odyssey Research Associates (page images at HathiTrust)
• Langley Research Center: Applications of power spectral analysis methods to maneuver loads obtained on jet fighter airplanes during service operations (National Aeronautics and Space Administration ;, 1961), also by John P. Mayer (page images at HathiTrust)
• Langley Research Center: Applications of the Hybrid Automated Reliability Predictor / c Salvatore J. Bavuso ... [et al.]. (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by Salvatore J. Bavuso (page images at HathiTrust)
• Langley Research Center: Applications of the theory of optimal control of distributed-parameter systems to structural optimization (National Aeronautics and Space Administration ;, 1972), also by Jean-Louis Pierre Armand and Stanford University (page images at HathiTrust)
• Langley Research Center: Applying modeling results in designing a global tropospheric experiment : proceedings of a working group meeting (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Working Group on the Application of Modeling Research Results to the Design of a Global Tropospheric Experiment and United States. Office of Space Science and Applications (page images at HathiTrust)
• Langley Research Center: An approximate analysis of unsteady vaporization near the stagnation point of blunt bodies (National Aeronautics and Space Administration, 1959), also by Leonard Roberts (page images at HathiTrust)
• Langley Research Center: An approximate analytical method for vortex-lift and center of pressure on the slender wing (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Xieyuan Yin, Grace C. Liu, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An approximate buckling analysis for rectangular orthotropic plates with centrally located cutouts (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Michael P. Nemeth, Eric R. Johnson, and Manuel Stein (page images at HathiTrust)
• Langley Research Center: Approximate composition and thermodynamic properties of nonionized nitrogen-oxygen mixtures (National Aeronautics and Space Administration, 1959), also by Richard A. Hord (page images at HathiTrust)
• Langley Research Center: Approximate indicial lift function for tapered, swept wings in incompressible flow (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by M. J. Queijo, Dinesh A. Keskar, William R. Wells, Cinncinnati. University, Wright State University, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: An approximate method for calculating three-dimensional inviscid hypersonic flow fields (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Christopher J. Riley and Fred R. DeJarnette (page images at HathiTrust)
• Langley Research Center: Approximate optimal guidance for the advanced launch system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), also by T. S. Feeley, J. L. Speyer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: An approximate solution for luminosity distance in zero-pressure relativistic model universes that have the U-property (National Aeronautics and Space Administration ;, 1965), also by Windsor L. Sherman (page images at HathiTrust)
• Langley Research Center: An approximate solution for the radar echo pulse response for planetary radar altimeters (National Aeronautics and Space Administration, 1971), also by W. Thomas Bundick and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An approximate theory for transverse shear deformation and rotatory inertia effects in vibrating beams (National Aeronautics and Space Administration ;, 1969), also by D. M. Egle, University of Oklahoma, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Approximate thermochemical tables for some C-H and C-H-O species (National Aeronautics and Space Administration ;, 1973), also by Gilbert S. Bahn and LTV Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Approximation methods for combined thermal/structural design (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Raphael T. Haftka, Charles P. Shore, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Approximation to the statistics of midcourse velocity corrections (National Aeronautics and Space Administration ;, 1969), also by Lawrence H. Hoffman, George R. Young, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Argon/UF6 plasma experiments : UF6 regeneration and product analysis (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Ward C. Roman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Arousal from sleep by noises from aircraft with and without acoustically treated nacelles (National Aeronautics and Space Administration ;, 1973), also by Jerome S. Lukas, Mary E. Dobbs, Donald J. Peeler, and Stanford Research Institute (page images at HathiTrust)
• Langley Research Center: Assessing the impact of modeling limits on intelligent systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by William B. Rouse, John M. Hammer, and Inc Search Technology (page images at HathiTrust)
• Langley Research Center: Assessment of a transitional boundary layer theory at low hypersonic mach numbers (National Aeronautics and Space Administration ;, 1972), also by S. J. Shamroth, H. McDonald, and United Aircraft Corporation (page images at HathiTrust)
• Langley Research Center: Assessment of carbon fiber electrical effects : an industry/government briefing held at Langley Research Center, Hampton, Virginia, December 4-5, 1979. (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Assessment of ground effects on aricraft noise : the T-38A flight experiment (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by William L. Willshire and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Assessment of space vehicle aeroacoustic- vibration prediction, design, and testing (National Aeronautics and Space Administration ;, 1970), also by Harry Himelblau, Terry D. Scharton, C. Myron Fuller, and McDonnell Douglas Astronautics Company-West (page images at HathiTrust)
• Langley Research Center: Assessment of techniques for measuring tropospheric HxOy : proceedings of a workshop sponsored by the NASA Office of Space Science and Applications, and NASA Langley Research Center, and held in Palo Alto, California August 16-20, 1982 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Calif.) Instrument Workshop for HxOy Tropospheric Species (1982 : Palo Alto, James M. Hoell, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and United States. Office of Space Science and Applications (page images at HathiTrust)
• Langley Research Center: Assessment of techniques for measuring tropospheric NxOy : proceedings of a workshop sponsored by the NASA Office of Space Science and Applications and NASA Langley Research Center and held in Palo Alto, California, August 16-20, 1982. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch and United States. Office of Space Science and Applications (page images at HathiTrust)
• Langley Research Center: An assessment of the accuracy of orthotropic photoelasticity (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), also by M. W. Hyer, D. H. Liu, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Assessment of turbulence models for scramjet flowfields (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by M. M. Sindir, P. T. Harsha, inc. Combustion Science and Advanced Technology Dept Science Applications, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An assessment of viscous effects in computational simulation of benign and burst vortex flows on generic fighter wind-tunnel models using TEAM code (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by Tim A. Kinard, Pradeep Raj, and Brenda W. Harris (page images at HathiTrust)
• Langley Research Center: Asymmetric hypersonic flow (National Aeronautics and Space Administration ;, 1972), also by Stephen H. Maslen and Md.) Research Institute for Advanced Study (Baltimore (page images at HathiTrust)
• Langley Research Center: Asymmetric lateral-directional characteristics of pointed bodies of revolution at high angles of attack (National Aeronautics and Space Administration ;, 1972), also by Paul L. Coe, William Letko, and Joseph R. Chambers (page images at HathiTrust)
• Langley Research Center: Asymmetric nonlinear dynamic response and buckling of shallow spherical shells (National Aeronautics and Space Administration ;, 1969), also by Atis A. Liepens and Dynatech Corporation (page images at HathiTrust)
• Langley Research Center: An asymptotic expansion approach to the inverse radiative transfer problem (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Richard I. Gomberg, James J. Buglia, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Atlas of wide-field-of-view outgoing longwave radiation derived from Nimbus 7 earth radiation budget data set : November 1985 to October 1987 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by T. Dale Bess and G. Louis Smith (page images at HathiTrust)
• Langley Research Center: Atmospheric entry and fragmentation of dense meteoroids (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by T. Dale Bess and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Atmospheric lidar multi-user instrument system definition study (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by R. V. Greco (page images at HathiTrust)
• Langley Research Center: Atmospheric neutrons (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Serge Alexander Korff and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Atmospheric rendezvous feasibility study (National Aeronautics and Space Administration ;, 1972), also by A. D. Schaezler and Vought Missiles and Space Company (page images at HathiTrust)
• Langley Research Center: Atmospheric solar absorption measurements in the 9 to 11 um region using a diode laser heterodyne spectrometer (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Charles N. Harward, James M. Hoell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Atmospheric studies related to aerospace activities and remote sensing technology (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by N. D. Sze and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Atomization, drop size, and penetration for cross-stream water injection at high-altitude reentry conditions with application to the RAM C-I and C-III flights (National Aeronautics and Space Administration ;, 1972), also by Paul B. Gooderum, Dennis M. Bushnell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Attitude-referenced radiometer study. Part II, Primary calibration system (National Aeronautics and Space Administration ;, 1971), also by William R. Williamson, Allen A. Otte, and Honeywell Inc (page images at HathiTrust)
• Langley Research Center: Attitude reorientation of spacecraft by means of impulse coning (National Aeronautics and Space Administration ;, 1977), also by C. William Martz and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Auger electron intensity variations in oxygen-charged large grain polycrystalline silver (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by W. S. Lee (page images at HathiTrust)
• Langley Research Center: An Auger electron spectroscopy study of surface-preparation contaminants (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by D. Wu (page images at HathiTrust)
• Langley Research Center: Automated decision making and problem solving (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Ewald Heer, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Conference on Automated Decision Making and Problem Solving (1980 : Langley Research Center) (page images at HathiTrust)
• Langley Research Center: Automated dynamic analytical model improvement (National Aeronatucs and Space Administration, Scientific and Technical Information Branch, 1981), also by Alex Berman, Fu Shang Wei, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Automated Mars surface sample return mission concepts for achievement of essential scientific objectives (National Aeronautics and Space Administration ;, 1975), also by William L. Weaver, Wayne L. Darnell, and Harry N. Norton (page images at HathiTrust)
• Langley Research Center: Automated procedure for design of wing structures to satisfy strength and flutter requirements (National Aeronautics and Space Administration ;, 1973), also by Raphael T. Haftka (page images at HathiTrust)
• Langley Research Center: Automatic guidance and control of a transport aircraft during a helical landing approach (National Aeronautics and Space Administration ;, 1975), also by Daniel J. Crawford and Roland L. Bowles (page images at HathiTrust)
• Langley Research Center: An automatic system for determining solar absorptance and thermal emittance of surfaces from spectral normal reflectance measurements (National Aeronautics and Space Administration ;, 1965), also by Louis A. Teichman and Harold D. Burks (page images at HathiTrust)
• Langley Research Center: Avionics and controls research and technology (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Duncan E. McIver, Herman A. Rediess, United States. Office of Aeronautics and Space Technology, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Awakening effects of simulated sonic booms and subsonic aircraft noise on six subjects, 7 to 72 years of age (National Aeronautics and Space Administration, 1970), also by Jerome S. Lukas, Karl D. Kryter, Stanford Research Institute, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Axisymmetric shell analysis of the space shuttle solid rocket booster field joint (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Michael P. Nemeth and Melvin S. Anderson (page images at HathiTrust)
• Langley Research Center: Background noise measurements from jet exit vanes designed to reduce flow pulsations in an open-jet wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Danny R. Hoad, R. M. Martin, and United States. Army Aviation Systems Command. Structures Laboratory (page images at HathiTrust)
• Langley Research Center: Bank-to-turn control technology survey for homing missiles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Frederick W. Riedel and Johns Hopkins University. Applied Physics Laboratory (page images at HathiTrust)
• Langley Research Center: Baseline experiments in teleoperator control (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1995), also by Walter W. Hankins, Randolph W. Mixon, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds (National Aeronautics and Space Administration, 1960), also by Robert S. Osborne, Virginia C. Stafford, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Behavior of aircraft antiskid braking systems on dry and wet runway surfaces : a slip-velocity-controlled, pressure-bias-modulated system (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1979), also by Sandy M. Stubbs, Eunice G. Smith, John A. Tanner, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Behavior of aircraft antiskid braking systems on dry and wet runway surfaces : a velocity-rat-controlled, pressure-bias-modulated system (National Aeronautics and Space Administration ;, 1976), also by Sandy M. Stubbs, John A. Tanner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Behavior of aircraft antiskid braking systems on dry and wet runway surfaces : hydromechanically controlled system (National Aeronautics and Space Administration, Scientific and Technical Information Branch :, 1981), also by John A. Tanner, Eunice G. Smith, Sandy M. Stubbs, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Benchmark solutions for the galactic heavy-ion transport equations with energy and spatial coupling (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Barry D. Ganapol (page images at HathiTrust)
• Langley Research Center: Benefits from synergies and advanced technologies for an advanced-technology space station (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by L. Bernard Garrett (page images at HathiTrust)
• Langley Research Center: Bibliography of supersonic cruise aircraft research (SCAR) program from 1972 to mid-1977 (National Aeronautics and Space Administration ;, 1977), also by Sherwood Hoffman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Bibliography of Supersonic Cruise Research (SCR) Program from 1977 to mid-1980 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Sherwood Hoffman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Biotechnology; proceedings. (Scientific and Technical Information Office, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1971), also by Conference on Biotechnology (1967 : Virginia Polytechnic Institute) and Virginia Polytechnic Institute (page images at HathiTrust)
• Langley Research Center: Blade-mounted trailing edge flap control for BVI noise reduction (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by A. A. Hassan and McDonnell Douglas Helicopter Company (page images at HathiTrust)
• Langley Research Center: BLSTA - a boundary layer code for stability analysis (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Yong-Sun Wie and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: Body motions and angles of attack during Project Fire flight II reentry (National Aeronautics and Space Administration ;, 1967), also by William I. Scallion and John H. Lewis (page images at HathiTrust)
• Langley Research Center: Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at Mach 2.50 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Jerry M. Allen, Milton Lamb, Gloria Hernandez, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A boundary element alternating method for two-dimensional mixed-mode fracture problems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by I. S. Raju, Thaiya Krishnamurthy, Inc Analytical Services & Materials, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: Boundary-layer electron profiles for entry of a blunt slender body at high altitude (National Aeronautics and Space Administration ;, 1973), also by John S. Evans, Paul W. Huber, and Charles J. Schnexnayder (page images at HathiTrust)
• Langley Research Center: Boundary-layer separation on isolated boattail nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by William Kelly Abeyounis and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Boundary layer stability on a yawed spinning body of revolution and its effect on the magnus force and moment (National Aeronautics and Space Administration ;, 1972), also by I. D. Jacobson, J. B. Morton, and University of Virginia (page images at HathiTrust)
• Langley Research Center: Boundary-layer transition and displacement-thickness effects on zero-lift drag of a series of power-law bodies at Mach 6 (National Aeronautics and Space Administration ;, 1974), also by George C. Ashby and Julius E. Harris (page images at HathiTrust)
• Langley Research Center: Boundary-layer velocity profiles downstream of three-dimensional transition trips on a flat plate at Mach 3 and 4 (National Aeronautics and Space Administration ;, 1969), also by John B. Peterson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Brazed Borsic/aluminum structural panels (National Aeronautics and Space Administration ;, 1977), also by Thomas T. Bales, Dick M. Royster, H. Ross Wiant, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Breakdown of the conservative potential equation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by M. D. Salas and Clyde R. Gumbert (page images at HathiTrust)
• Langley Research Center: A brief study of closed-circuit television for aircraft landing (National Aeronautics and Space Administration :, 1964), also by John P. Reeder and Joseph J. Kolnick (page images at HathiTrust)
• Langley Research Center: A brief study of the effects of turbofan-engine bypass ratio on short- and long-haul cruise aircraft (National Aeronautics and Space Administration ;, 1975), also by Arvid L. Keith (page images at HathiTrust)
• Langley Research Center: Broadband noise generated by turbulent inflow to rotor or stator blades in an annular duct (National Aeronautics and Space Administration ;, 1975), also by Frank Lane and KLD Associates (page images at HathiTrust)
• Langley Research Center: Broadband rotor noise analyses (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), also by Albert R. George, Shau-Tak Chou, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Broken symmetry in ideal magnetohydrodynamic turbulence (National Aeronautics and Space Administration, Langley Research Center ;, 1993), also by John V. Shebalin (page images at HathiTrust)
• Langley Research Center: Bubble Memory Module (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by O. D. Bohning, F. J. Becker, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Buckling analysis for axially compressed flat plates, structural sections, and stiffened plates reinforced with laminated composites (National Aeronautics and Space Administration ;, 1971), also by A. V. Viswanathan, R. E. Miller, Tsai-Chen Soong, and Boeing Company (page images at HathiTrust)
• Langley Research Center: A buckling analysis for rectangular orthotropic plates with centrally located cutouts (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Michael P. Nemeth (page images at HathiTrust)
• Langley Research Center: The buckling analysis of imperfection sensitive shell structures / Johann Arbocz and Charles D. Babcock, Jr. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Johann Arbocz, Charles D. Babcock, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Buckling and postbuckling behavior of compression-loaded isotropic plates with cutouts (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Michael P. Nemeth (page images at HathiTrust)
• Langley Research Center: Buckling and postbuckling behavior of square compression-loaded graphite-expoxy plates with circular cutouts (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Michael P. Nemeth (page images at HathiTrust)
• Langley Research Center: Buckling and structural efficiency of sandwich-blade stiffened composite compression panels (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Manuel Stein, Jerry G. Williams, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Buckling and vibration analysis of a simply supported column with a piecewise constant cross section (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Mark S. Lake and Martin M. Mikulas (page images at HathiTrust)
• Langley Research Center: Buckling behavior of long symmetrically laminated plates subjected to combined loadings (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Michael P. Nemeth (page images at HathiTrust)
• Langley Research Center: Buckling of conical shell with local imperfections (National Aeronautics and Space Administration ;, 1974), also by Paul A. Cooper and Cornelia B. Dexter (page images at HathiTrust)
• Langley Research Center: Buckling test of a 3-meter-diameter corrugated graphite-epoxy ring-stiffened cylinder (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Randall C. Davis and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Buckling tests of three 4.6 meter diameter aluminum honeycomb sandwich conical shells loaded under external pressure (National Aeronautics and Space Administration ;, 1975), also by James Kent Anderson and Randall C. Davis (page images at HathiTrust)
• Langley Research Center: Buckling tests of two 4.6-meter-diameter, magnesium ring-stiffened conical shells loaded under external pressure (National Aeronautics and Space Administration ;, 1973), also by James Kent Anderson, Randall C. Davis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Buckling tests of two integrally stiffened cylinders subjected to bending (National Aeronautics and Space Administration ;, 1971), also by James Kent Anderson, James P. Peterson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Bumblebee Program - aerodynamic data (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by G. A. Barnes, L. L. Cronovich, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Bumper-protected laminated spacecraft mainwalls (National Aeronautics and Space Administration ;, 1971), also by Ray Kinslow and Tennessee Technological University (page images at HathiTrust)
• Langley Research Center: A buoyant tornado-probe concept incorporating an inverted lifting device (National Aeronautics and Space Administration ;, 1973), also by Frederick C. Grant and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Calculated effects of body shape on the bow-shock overpressures in the far field of bodies in supersonic flow (U.S. G.P.O., 1960), also by Donald L. Lansing and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Calculated radio attenuation due to plasma sheath on hypersonic blunt-nosed cone (National Aeronautics and Space Administration, 1963), also by John S. Evans and Paul W. Huber (page images at HathiTrust)
• Langley Research Center: Calculated responses of a large sweptwing airplane to continuous turbulence with flight-test comparisons (U.S. G.P.O., 1960), also by Floyd V. Bennett, Kermit G. Pratt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Calculated wind-tunnel-boundary lift-interference factors for rectangular perforated test sections (National Aeronautics and Space Administration ;, 1970), also by Benferd L. Schilling and Ray H. Wright (page images at HathiTrust)
• Langley Research Center: Calculation of aerodynamic characteristics of airplane configurations at high angles of attack (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Jing-Biau Tseng and C. Edward Lan (page images at HathiTrust)
• Langley Research Center: Calculation of composition distribution of ultrafine ion-H₂O-H₂SO₄ clusters using a modified binary ion-nucleation theory (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Jag J. Singh and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Calculation of compressible, nonadiabatic boundary layers in laminar, transitional and turbulent flow by the method of integral relations (National Aeronautics and Space Administration, 1971), also by Gary D. Kuhn, United States. National Aeronautical and Space Administration, and Nielsen Engineering & Research (page images at HathiTrust)
• Langley Research Center: Calculation of electron energy deposition in thin-film polymeric materials (National Aeronautics and Space Administration, 1963), also by Louis A. Teichman and Ernest S. Armstrong (page images at HathiTrust)
• Langley Research Center: Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by H. Harris Hamilton and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Calculation of symmetric and asymmetric vortex separation on cones and tangent ogives based on discrete vortex models (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by S. Chin and C. Edward Lan (page images at HathiTrust)
• Langley Research Center: Calculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight tests (National Aeronautics and Space Administration, 1968), also by Joseph R. Chambers, Sue B. Grafton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The calculation of the eigenvalues and eigenfunctions of Mathieu's equation (National Aeronautics and Space Administration ;, 1972), also by D. B. Hodge and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: Calculation of the longitudinal aerodynamic characteristics of wing-flap configurations with externally blown flaps (National Aeronautics and Space Administration ;, 1976), also by M. R. Mendenhall and Nielsen Engineering & Research (page images at HathiTrust)
• Langley Research Center: Calculation of the penetration flux for a multiwall structure on the Lunar Orbiter spacecraft (National Aeronautics and Space Administration ;, 1969), also by Donald H. Humes and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Calculation of the twist distribution of wings designed for cruise at transonic speeds (National Aeronautics and Space Administration ;, 1974), also by Michael J. Mann (page images at HathiTrust)
• Langley Research Center: Calculation of three-dimensional, inviscid supersonic, steady flows (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), also by Gino Moretti, Polytechnic Institute of New York, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. Part 1, Summary report (National Aeronautics and Space Administration ;, 1971), also by C. Economos, J. Boccio, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Langley Research Center: Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. Part II, Constant property turbulent boundary layer flow with simultaneous mass transfer and pressure gradient (National Aeronautics and Space Administration ;, 1972), also by J. Boccio, C. Economos, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Langley Research Center: Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. Part III, Computer program manual (National Aeronautics and Space Administration ;, 1972), also by J. Schneider, J. Boccio, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Langley Research Center: Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects - program documentation and test case (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Sedat Biringen, Oden J. McMillan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects : User's manual (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Sedat Biringen, Oden J. McMillan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Calculation of two-dimensional inlet flow fields in a supersonic free stream : program documentation and test cases (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Sedat Biringen, Oden J. McMillan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Calculation of two-dimensional inlet flow fields in a supersonic free strem by an implicit marching code with nonorthogonal mesh generation : user's manual (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Sedat Biringen, Oden J. McMillan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Calculation of two-neutron multiplicity in photonuclear reactions (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by John W. Norbury and Lawrence W. Townsend (page images at HathiTrust)
• Langley Research Center: Calculation of unsteady transonic aerodynamics for oscillating wings with thickness (National Aeronautics and Space Administration ;, 1975), also by S. Y. Ruo, J. G. Theisen, and Lockheed-Georgia Company (page images at HathiTrust)
• Langley Research Center: Calculation of unsteady transonic flows with mild separation by viscous-inviscid interaction (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by James T. Howlett (page images at HathiTrust)
• Langley Research Center: Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by James T. Howlett and Samuel R. Bland (page images at HathiTrust)
• Langley Research Center: Calculation of vortex lift effect for cambered wings by the suction analogy (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by C. Edward Lan, Jen-Fu Chang, University of Kansas. Center for Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Calculation of wind-driven surface currents in the North Atlantic Ocean (National Aeronautics and Space Administration ;, 1976), also by Thomas H. Rees and Richard E. Turner (page images at HathiTrust)
• Langley Research Center: Calibration of sonic valves for the laminar flow control, leading-edge flight test (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by D. H. Petley (page images at HathiTrust)
• Langley Research Center: Calibration of the 13- by 13-inch adaptive wall test section for the Langley O.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Raymond E. Mineck and Acquilla S. Hill (page images at HathiTrust)
• Langley Research Center: Calibration of the Langley 16-foot transonic tunnel with test section air removal (National Aeronautics and Space Administration ;, 1974), also by Blake W. Corson, William B. Igoe, and Jack F. Runckel (page images at HathiTrust)
• Langley Research Center: Calibration of the Spin-Scan Ozone Imager aboard the Dynamics Explorer 1 satellite (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Walter E. Bressette, Dave Fryer Young, and Gerald M. Keating (page images at HathiTrust)
• Langley Research Center: Calorimetric evaluation of two cone-column solar-energy concentrators (National Aeronautics and Space Administration ;, 1969), also by Marvin D. Rhodes, Conrad M. Willis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Capacitance discharge system for ignition of Single Bridge Apollo Standard Initiators (SBASI) (National Aeronautics and Space Administration ;, 1974), also by R. D. Ward and LTV Aerospace Corporation. Vought Systems Division (page images at HathiTrust)
• Langley Research Center: Carbide coated fibers in graphite-aluminum composites (U.S. National Aeronautics and Space Administration ;, 1976), also by Richard J. Imprescia, United States National Aeronautics and Space Administration, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Langley Research Center: Carbide coated fibers in graphite-aluminum composites : progress report (National Aeronautics and Space Administration ;, 1975), also by Richard J. Imprescia and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Langley Research Center: Carbon fiber risk analysis. (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: CARE III phase II report : mathematical description (National Aeronautics and Space Administration, Scientific And Technical Information Branch ;, 1982), also by J. J. Stiffler, L. A. Bryant, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Raytheon Company, and Air Force Avionics Laboratory (page images at HathiTrust)
• Langley Research Center: CARE III phase III report : test and evaluation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by J. J. Stiffler, L. A. Bryant, J. S. Neumann, Raytheon Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Cellular repair/misrepair track model (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by John W. Wilson and Francis A. Cucinotta (page images at HathiTrust)
• Langley Research Center: Cellular track model of biological damage to mammalian cell cultures from galactic cosmic rays (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Francis A. Cucinotta (page images at HathiTrust)
• Langley Research Center: CERES : Clouds and the Earth's radiant energy system : NASA's earth observing system (NASA Langley Research Center, 1999) (page images at HathiTrust)
• Langley Research Center: Certification methodology for stiffener terminations (Federal Aviation Administration, Office of Aviation Research ;, 1996), also by C. H. Shah, M. Mahler, H. P. Kan, Northrop Corporation. Military Aircraft Division, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Langley Research Center: Characteristics of capacitor-type micrometeoroid flux detectors when impacted with simulated micrometeoroids (National Aeronautics and Space Administration ;, 1973), also by Philip C. Kassel (page images at HathiTrust)
• Langley Research Center: Characteristics of Mach 10 transitional and turbulent boundary layers (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Ralph D. Watson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Characteristics of major active wind tunnels at the Langley Research Center (National Aeronautics and Space Administration ;, 1965), also by William T. Schaefer (page images at HathiTrust)
• Langley Research Center: Characterization of real-time computers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Kang G. Shin, C. M. Krishna, University of Michigan. Dept. of Electrical and Computer Engineering, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Characterization, parameter estimation, and aircraft response statistics of atmospheric turbulence (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by William D. Mark and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Charge storage effects in mylar resulting from electron irraiation (National Aeronautics and Space Administration ;, 1966), also by L. K. Monteith, Research Triangle Institute, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Charge-to-mass dispersion methods for abrasion-ablation fragmentation models (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Lawrence W. Townsend and John W. Norbury (page images at HathiTrust)
• Langley Research Center: Charts depicting kinematic and heating parameters for a ballistic reentry at speeds of 26,000 to 45,000 feet per second (National Aeronautics and Space Administration, 1961), also by Uriel M. Lovelace and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Charts for determing potential minimum sonic-boom overpressures for supersonic cruise aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Christine M. Darden and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Charts for equilibrium isentropic expansion of air behind shocks up to 50,000 per second (15.24 kilometers per second) (National Aeronautics and Space Administration ;, 1967), also by Ernest V. Zoby and Wayne D. Erickson (page images at HathiTrust)
• Langley Research Center: Charts for predicting the subsonic vortex-lift characteristics of arrow, delta, and diamond wings (National Aeronautics and Space Administration ;, 1971), also by Edward C. Polhamus and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Chemical equilibrium of ablation materials including condensed species (National Aeronautics and Space Administration ;, 1969), also by C. W. Stroud, Kay L. Brinkley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Chemical impurity data on selected artificial graphites with comments on the catalytic effect of impurities on oxidation rate (National Aeronautics and Space Administration ;, 1967), also by Howard G. Maahs and David R. Schryer (page images at HathiTrust)
• Langley Research Center: Chemical kinetic analysis of hydrogen-air ignition and reaction times (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by R. Clayton Rogers, Charles J. Schexnayder, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Chemical kinetic modeling of benzene and toluene oxidation behind shock waves (National Aeronautics and Space Administration ;, 1979), also by Allen G. McLain, Charles H. Wilson, Casimir J. Jachimowski, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Chemical kinetic models for combustion of hydrocarbons and formation of nitric oxide (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Casimir J. Jachimowski, Charles H. Wilson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Chemical nonequilibrium effects on the inviscid flow in the windward plane of symmetry of two simplified shuttle configurations (National Aeronautics and Space Administration ;, 1973), also by John A. Lordi, Charles B. Johnson, and Robert J. Vidal (page images at HathiTrust)
• Langley Research Center: The chemical/physical and microbiological characteristics of typical bath and laundry waste waters (National Aeronautics and Space Administration ;, 1974), also by Warren D. Hypes, Judd Rice Wilkins, and Carmen E. Batten (page images at HathiTrust)
• Langley Research Center: Chesapeake Bay Plume Study : superflux 1980 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by James P Thomas, Janet W Campbell, Northeast Fisheries Center (U.S.), and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Circuit transients due to negative bias arcs on a high-voltage solar array in low earth orbit (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Roger N. Metz and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Close-range photogrammetric measurement of static deflections for an aeroelastic superficial wing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Thomas A. Byrdsong, M. C. Sandford, and Richard R. Adams (page images at HathiTrust)
• Langley Research Center: Closed-cycle, frequency-stable CO2 laser technology (National Aeronautics and Space Administration, 1987), also by Frequency-Stable CO2 Laser Technology Workshop on Closed-cycle, Carmen E. Batten, United States National Aeronautics and Space Administration, and Royal Signals and Radar Establishment (Great Britain) (page images at HathiTrust)
• Langley Research Center: Closed loop models for analyzing engineering requirements for simulators (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Sheldon Baron, David L. Kleinman, Ramal Muralidharan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Coatings and surface treatments for longtime protection of Ti-8Al-1Mo-1V alloy sheet from hot-salt stress corrosion (National Aeronautics and Space Administration ;, 1968), also by Bland A. Stein, Dick M. Royster, and H. Benson Dexter (page images at HathiTrust)
• Langley Research Center: A cockpit-display concept for executing a multiple glide-slope approach for wake-vortex avoidance (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Terence S. Abbott (page images at HathiTrust)
• Langley Research Center: Cockpit Ocular Recording System (CORS) (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Edward Rothenheber and Inc Analytics (page images at HathiTrust)
• Langley Research Center: Collected papers on instability of shell structure, 1962 (National Aeronautics and Space Administration, 1962), also by NASA Symposium on Instability of Shell Structures (1962 : Langley Research Center) and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Collected papers on instability of shell structures, 1962. (National Aeronautics and Space Administration, 1962), also by NASA Symposium on Instability of Shell Structures (1962 : Langley Research Center) and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Collective motions of a one-dimensional self-gravitating system (National Aeronautics and Space Administration ;, 1969), also by Frank Hohl, Janet W. Campbell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Collisionless galaxy simulations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Frank Hohl, John B. Miller, Thomas A. Zang, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Collisionless relaxation in spiral galaxy models (National Aeronautics and Space Administration ;, 1974), also by Frank Hohl (page images at HathiTrust)
• Langley Research Center: The combined influence of molecular weight and temperature on the aging and viscoelastic response of a glassy thermoplastic polyimide (National Aeronautics and Space Administration, Langley Research Center, 2000), also by Lee M. Nicholson, Thomas S. Gates, and Karen S. Whitley (page images at HathiTrust)
• Langley Research Center: Combined linear theory/impact theory for analysis and design of high speed configurations (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), also by D. Brooke, McDonnell Aircraft Company, and D. V. Vondrasek (page images at HathiTrust)
• Langley Research Center: Combined single-pulse holography and time-resolved laser schlieren for flow visualization (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Alpheus W. Burner, William K. Goad, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A combined stochastic feedforward and feedback control design methodology with application to autoland design (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987), also by Nesim Halyo (page images at HathiTrust)
• Langley Research Center: Combustion contribution to noise in jet engines (U.S. National Aeronautics and Space Administration ;, 1976), also by E. G. Plett, United States National Aeronautics and Space Administration, and Princeton University (page images at HathiTrust)
• Langley Research Center: Combustion of hydrogen-air jets in local chemical equilibrium : (a guide to the CHARNAL computer program) (National Aeronautics and Space Administration ;, 1974), also by D. B. Spalding and Fluid Mechanics and Thermal Systems (page images at HathiTrust)
• Langley Research Center: Comments on several reduced-gravity simulators used for studying lunar self-locomotive tasks (National Aeronautics and Space Administration, 1970), also by Amos A. Spady and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A commercial airport noise environment : measurement, prediction and control (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by J. E. Mabry, B. M. Sullivan, inc Man-Acoustics and Noise, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Community sensitivity to changes in aircraft noise exposure (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by S. A. Fidell, Beranek Bolt, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Comparative analyses of space-to-space central power stations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Paul F. Holloway, L. Bernard Garrett, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Comparative performance of HgCdTe photodiodes for heterodyne application (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Herbert R. Kowitz and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A comparative study of the nonuniqueness problem of the potential equation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by M. D. Salas, R. E. Melnik, and A. Jameson (page images at HathiTrust)
• Langley Research Center: Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Raymond E. Mineck (page images at HathiTrust)
• Langley Research Center: Comparison of acoustic performance of five muffler configurations on a small helicopter (National Aeronautics and Space Administration ;, 1974), also by Robert J. Pegg and David A. Hilton (page images at HathiTrust)
• Langley Research Center: A comparison of airborne wake vortex detection measurements with values predicted from potential theory (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Eric C. Stewart (page images at HathiTrust)
• Langley Research Center: Comparison of analytical and flight test identified aerodynamic derivatives for a tandem-rotor transport helicopter (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Ward F. Hodge and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Comparison of analytical and wind-tunnel results for flutter and gust response of a transport wing with active controls (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Irving Abel, Jerry R. Newsom, Boyd Perry, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Comparison of analytical predictions of longitudinal short-period pilot-induced oscillations with results from a simulation study of the space shuttle orbiter (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Donald R. Riley, G. Kimball Miller, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Comparison of data inversion techniques for remotely sensed wide-angle observations of earth emitted radiation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Richard N. Green and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Comparison of dose estimates using the buildup-factor method and a baryon transport code (BRYNTRN) with Monte Carlo results (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Judy L. Shinn (page images at HathiTrust)
• Langley Research Center: Comparison of exact and approximate evaluations of the single-scattering integral in nucleon-deuteron elastic scattering (National Aeronautics and Space Administration ;, 1972), also by John W. Wilson (page images at HathiTrust)
• Langley Research Center: Comparison of experimental and theoretical static aeroelastic loads and deflections of a thin 45° wing in supersonic flow (National Aeronautical and Space Administration, 1961), also by Floyd V. Bennett and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Comparison of experimental and theoretical turbulance reduction characteristics for screens, honeycomb, and honeycomb-screen combinations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by James Scheiman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Comparison of finite-difference schemes for analysis of shells of revolution (National Aeronautics and Space Administration ;, 1973), also by Ahmed Khairy Noor, Wendell B. Stephens, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Comparison of flying qualities derived from in-flight and ground-based simulators for a jet-transport airplane for the approach and landing pilot tasks (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by William D. Grantham (page images at HathiTrust)
• Langley Research Center: Comparison of foward flight effects theory of A. Michalke and U. Michel with measured data (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by John W. Rawls, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Kentron International (page images at HathiTrust)
• Langley Research Center: Comparison of full-scale and model buffet response of Apollo boilerplate service module (National Aeronautics and Space Administration ;, 1966), also by Robert V. Doggett (page images at HathiTrust)
• Langley Research Center: Comparison of full-scale lift and drag characteristics of the x-15 airplane with wind-tunnel results and theory (National Aeronautics and Space Administration, 1962), also by Edward J. Hopkins, Edwin J. Saltzman, David E. Fetterman, Flight Research Center (U.S.), and Ames Research Center (page images at HathiTrust)
• Langley Research Center: Comparison of genetic algorithms with conjugate gradient methods (National Aeronautics and Space Administration ;, 1972), also by Jack Bosworth, Bernard P. Zeigler, N. Y. Foo, and University of Michigan (page images at HathiTrust)
• Langley Research Center: A comparison of graphite/epoxy tape laminates and 2-D braided composites mechanical properties (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Pierre J. Minguet and Christian K. Gunther (page images at HathiTrust)
• Langley Research Center: Comparison of hinge moments for a simple delta wing and a delta-wing orbiter concept at mach 6 (National Aeronautics and Space Administration, 1972), also by George C. Ashby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Comparison of information display concepts for landing of VTOL aircraft (National Aeronautics and Space Administration, 1968), also by William Gracey and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Comparison of jet plume shape predictions and plume influence on sonic boom signature (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Raymond L. Barger and N. Duane Melson (page images at HathiTrust)
• Langley Research Center: Comparison of low-frequency noise levels of the Concorde supersonic transport with other commercial service airplanes (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Clemans A. Powell, David A. McCurdy, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A comparison of matrix methods for calculating eigenvalues in acoustically lined ducts (U.S. National Aeronautics and Space Administration ;, 1976), also by Willie Watson and Donald L. Lansing (page images at HathiTrust)
• Langley Research Center: Comparison of measured and calculated sonic-boom ground patterns due to several different aircraft maneuvers (National Aeronautics and Space Administration, 1965), also by Donald L. Lansing, Domenic J. Maglieri, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Comparison of measured and calculated velocity profiles of a laminar incompressible free jet at low Reynolds numbers (National Aeronautics and Space Administration ;, 1974), also by George C. Greene (page images at HathiTrust)
• Langley Research Center: A comparison of measured and predicted sphere shock shapes in hypersonic flows with density ratios from 4 to 19 (National Aeronautics and Space Administration ;, 1975), also by Charles G. Miller (page images at HathiTrust)
• Langley Research Center: A comparison of measured and predicted test flow in an expansion tube with air and oxygen test gases (National Aeronautics and Space Administration ;, 1975), also by Kenneth V. Haggard and William K. Goad (page images at HathiTrust)
• Langley Research Center: Comparison of polyester, film-yarn composite, balloon materials subjected to shear and biaxial loading (National Aeronautics and Space Administration ;, 1972), also by R. J. Niccum and G.T. Schjeldahl Company (page images at HathiTrust)
• Langley Research Center: Comparison of predicted and experimental real-gas pressure distributions on Space Shuttle Orbiter nose for Shuttle Entry Air Data System (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Judy L. Shinn and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A comparison of results from two simulators used for studies of astronaut maneuvering units (National Aeronautics and Space Administration ;, 1973), also by Eric C. Stewart and Robert L. Cannaday (page images at HathiTrust)
• Langley Research Center: Comparison of several methods for estimating low-speed stability derivatives for two airplane configurations (National Aeronautics and Space Administration ;, 1971), also by Herman S. Fletcher and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Delma C. Freeman, Bernard Spencer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Comparison of steady-state and six-degree-of-freedom analyses of pitch-roll resonance conditions for a long slender sounding rocket (National Aeronautics and Space Administration, 1963), also by Charles H. Whitlock and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Comparison of structural performance of one- and two-bay rotary joints for truss applications (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by J. Douglas Vail and Mark S. Lake (page images at HathiTrust)
• Langley Research Center: A comparison of superconductor and manganin technology for electronic links used in space mission applications (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by R. Caton, A. M. Buoncristiani, R. Selim, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: A comparison of techniques for inversion of radio-ray phase data in presence of ray bending (National Aeronautics and Space Administration ;, 1972), also by H. Andrew Wallio and Mario D. Grossi (page images at HathiTrust)
• Langley Research Center: A comparison of the noise produced by a small jet on a moving vehicle with that in a free jet (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Thomas D. Norum and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A comparison of the pitching and plunging response of an oscillating airfoil (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by F. O. Carta and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Comparison of thin-film resistance heat-transfer gages with thin-skin transient calorimeter gages in conventional hypersonic wind tunnels (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Charles G. Miller and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Comparison of two computer programs by predicting turbulent mixing of helium in a ducted supersonic airstream (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Y. S. Pan, Charles R. McClinton, John Philip Drummond, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Comparison of various methods of mathematical analysis of the Foucault knife-edge test pattern to determine optical imperfections (National Aeronautics and Space Administration ;, 1971), also by Buford Echols Gatewood and Ohio State University. Research Foundation (page images at HathiTrust)
• Langley Research Center: Comparison of VGH data from wide-body and narrow-body long-haul turbine-powered transports (National Aeronautics and Space Administration ;, 1977), also by John A. Zalovcik, Garland J. Morris, Joseph W. Jewel, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Comparison of vibrations of a combination of solid-rocket launch vehicle and payload during a ground firing and launching (National Aeronautics and Space Administration ;, 1975), also by James A. Schoenster and Harold B. Pierce (page images at HathiTrust)
• Langley Research Center: Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method (National Aeronautics and Space Administration ;, 1975), also by Larry Wayne Mohn and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Jacob H. Lichtenstein and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Comparisons of theoretical and experimental pressure distributions over a wing-body model at high supersonic speeds (National Aeronautics and Space Administration ;, 1971), also by Lloyd S. Jernell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Comparisons of two-dimensional shock-expansion theory with experimental aerodynamic data for delta-planform wings at high supersonic speeds (National Aeronautics and Space Administration ;, 1974), also by Lloyd S. Jernell (page images at HathiTrust)
• Langley Research Center: Compendium of NASA data base for the Global Tropospheric Experiment's Pacific Exploratory Mission -- Tropics B (PEM-Tropics B) (National Aeronautics and Space Administration, Langley Research Center, 2000), also by A. Donald Scott, James L. Raper, and Mary M. Kleb (page images at HathiTrust)
• Langley Research Center: Compensation based on linearized analysis for a six-degree-of-freedom motion simulator (National Aeronautics and Space Administration ;, 1973), also by Russell V. Parrish, James L. Copeland, Dennis J. Martin, James E. Dieudonne, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A compensatory algorithm for the slow-down effect on constant-time-separation approaches (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Terence S. Abbott (page images at HathiTrust)
• Langley Research Center: A compilation and analysis of typical approach and landing data for a simulator study of an externally blown flap STOL aircraft (National Aeronautics and Space Administration ;, 1974), also by David B. Middleton and Hugh P. Bergeron (page images at HathiTrust)
• Langley Research Center: Complex permittivity measurements during high temperature recycling of space shuttle antenna window and dielectric heat shield materials (National Aeronautics and Space Administration ;, 1973), also by Harold L. Bassett, S. H. Bomar, and Georgia Institute of Technology (page images at HathiTrust)
• Langley Research Center: Composite engines for application to a single-stage-to-orbit vehicle (National Aeronautics and Space Administration ;, 1975), also by Joseph G. Bendot, Thomas G. Piercy, Philip N. Brown, and Marquardt Company (page images at HathiTrust)
• Langley Research Center: Composite materials flown on the long duration exposure facility (National Aeronautics and Space Administration, Langley Research Center, 1995), also by Pete E. George, H. Gary Pippin, and Harry Dursch (page images at HathiTrust)
• Langley Research Center: Composite materials for rail transit systems (National Aeronautics and Space Administration, Langley Research Center, 1988), also by Carl T. Herakovich, Zafer Gürdal, O. Hayden Griffin, United States. Urban Mass Transportation Administration, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Langley Research Center: Compressibility effects on the hovering performance of a two-blade 10-foot-diameter helicopter rotor operating at tip Mach numbers up to 0.98 (National Aeronautics and Space Administration, 1960), also by Joesph W. Jewel (page images at HathiTrust)
• Langley Research Center: The compressible turbulent boundary layer on a blunt swept slab with and without leading-edge blowing (National Aeronautics and Space Administration ;, 1971), also by James L. Hunt, Ivan E. Beckwith, Dennis M. Bushnell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Compressible turbulent boundary layers; a symposium held at Langley Research Center, Hampton, Virginia, December 10-11, 1968. (Scientific and Technical Information Division, National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1969) (page images at HathiTrust; US access only)
• Langley Research Center: Compressible, unsteady lifting-surface theory for a helicopter rotor in forward flight (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Harry L. Runyan and H. Tai (page images at HathiTrust)
• Langley Research Center: Compression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Dawn C. Jegley (page images at HathiTrust)
• Langley Research Center: Compressive and tensile creep of 7075-T6 and 2024-T3 aluminum-alloy sheet (National Aeronautics and Space Administration, 1959), also by George J. Heimerl and John Farquhar (page images at HathiTrust)
• Langley Research Center: Compressive behavior of titanium alloy skin-stiffener specimens selectively reinforced with boron-aluminum composite (National Aeronautics and Space Administration :, 1971), also by Harvey W. Herring, Rosa C. Webster, Robert L. Carri, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings (National Aeronautics and Space Administration ;, 1975), also by W. H. Weatherill, James D. Sebastian, F. Edward Ehlers, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Theodore A. Reyhner, Boeing Commercial Airplane Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Computation of turbulent boundary layers employing the defect wall-function method (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Douglas L. Brown (page images at HathiTrust)
• Langley Research Center: Computational aspects of sensitivity calculations in linear transient structural analysis (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by William H. Greene (page images at HathiTrust)
• Langley Research Center: A computational examination of directional stability for smooth and chined forebodies at high-[alaph] (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Ramakrishnan Ravi, William H. Mason, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: A computational method for time-optimal space rendezvous (National Aeronautics and Space Administration ;, 1969), also by Ernest S. Armstrong and Athena T. Markos (page images at HathiTrust)
• Langley Research Center: Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by S. Venkateswaran, Ramadas K. Prabhu, and L. Roane Hunt (page images at HathiTrust)
• Langley Research Center: Computational methods for analyzing the transmission characteristics of a Beta Particle magnetic analysis system (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Jag J. Singh, Gerald H. Mall, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Computational methods for crashworthiness : proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington, D.C., and the University of Virginia Center for Computational Structures Technology, Hampton, Virginia, and held at Langley Research Center, Hampton, Virginia, September 2-3, 1992 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), also by Va.) Workshop on Computational Methods for Crashworthiness (1992 : Hampton, Huey D. Carden, Ahmed Khairy Noor, University of Virginia. Center for Computational Structures Technology, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Computational methods for frictionless contact with application to space shuttle orbiter nose-gear tires (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Kyun O. Kim (page images at HathiTrust)
• Langley Research Center: Computational methods for structural mechanics and dynamics : proceedings of a workshop sponsored by the National Aeronautics and Space Administration and held at NASA Langley Research Center, Hampton, Virginia, June 19-21, 1985 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989), also by W. Jefferson Stroud and Workshop on Computational Methods for Structural Mechanics and Dynamics (1985 : NASA Langley Research Center) (page images at HathiTrust)
• Langley Research Center: Computational methods in the prediction of advanced subsonic and supersonic propeller induced noise--ASSPIN user's manual (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by M. H. Dunn, G. M. Tarkenton, and Lockheed Engineering & Sciences Company (page images at HathiTrust)
• Langley Research Center: A computational model for the prediction of jet entrainment in the vicinity of nozzle boattails (The BOAT code) (National Aeronautics and Space Administration, Scientific and Technical Information Service ;, 1978), also by Sanford M. Dash, Harold S. Pergament, Aeronautical Research Associates of Princeton, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Computational structures technology for airframes and propulsion systems : proceedings of two workshops sponsored by the National Aeronautics and Space Administration, Washington, D.C., and the Center for Computational Structures Technology, University of Virginia, Hampton, Virginia, and held at Lewis Research Center, Cleveland, Ohio, June 26-27, 1991, and at Langley Research Center, Hampton, Virginia, September 4-5, 1991 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Ahmed Khairy Noor, University of Virginia. Center for Computational Structures Technology, United States National Aeronautics and Space Administration, Workshop on Computational Structures Technology for Airframes and Propulsion Systems (1991 : Langley Research Center), and Workshop on Computational Structures Technology for Airframes and Propulsion Systems (1991 : Lewis Research Center) (page images at HathiTrust)
• Langley Research Center: A computational system for aerodynamic design and analysis of supersonic aircraft : part 1-general description and theoretical development (U.S. National Aeronautics and Space Administration ;, 1976), also by W. D. Middleton, J. L. Lundry, United States National Aeronautics and Space Administration, and Boeing Company (page images at HathiTrust)
• Langley Research Center: A computational system for aerodynamic design and analysis of supersonic aircraft : part 3-computer program description (U.S. National Aeronautics and Space Administration ;, 1976), also by W. D. Middleton, Robert Griffin Coleman, J. L. Lundry, United States National Aeronautics and Space Administration, and Boeing Company (page images at HathiTrust)
• Langley Research Center: Computational tools and facilities for the next-generation analysis and design environment (National Aeronautics and Space Administration, Langley Research Center, 1997), also by Va.) Workshop on Computational Tools and Facilities for the Next Generation Analysis and Design Environment (1996 : Hampton, John B. Malone, Ahmed Khairy Noor, University of Virginia. Center for Advanced Computational Technology, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Computations for large, uniform circular arrays with typical element patterns (National Aeronautics and Space Administration :, 1964), also by C. R. Cockrell (page images at HathiTrust)
• Langley Research Center: Computed lateral power spectral density response of conventional and STOL airplanes to random atmospheric turbulence (National Aeronautics and Space Administration ;, 1974), also by Jacob H. Lichtenstein (page images at HathiTrust)
• Langley Research Center: Computed lateral rate and acceleration power spectral response of conventional and STOL airplanes to atmospheric turbulence (National Aeronautics and Space Administration ;, 1975), also by Jacob H. Lichtenstein (page images at HathiTrust)
• Langley Research Center: Computer-aided space shuttle orbiter wing design study (National Aeronautics and Space Administration ;, 1974), also by W. Pelham Phillips (page images at HathiTrust)
• Langley Research Center: Computer analysis of flow pertubations generated by placement of choke bumps in a wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Richard L. Campbell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Computer analysis of multicircuit shells of revolution by the field method (National Aeronautics and Space Administration ;, 1975), also by Gerald A. Cohen and Structures Research Associates (page images at HathiTrust)
• Langley Research Center: Computer analysis of ring-stiffened shells of revolution (National Aeronautics and Space Administration ;, 1973), also by Gerald A. Cohen and Structures Research Associates (page images at HathiTrust)
• Langley Research Center: Computer-automated opponent for manned air-to-air combat situations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Walter W. Hankins and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Computer experiments on the structure and dynamics of spiral galaxies (National Aeronautics and Space Administration ;, 1972), also by Frank Hohl and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Computer program BL2D for solving two-dimensional and axisymmetric boundary layers (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by Venkit Iyer (page images at HathiTrust)
• Langley Research Center: Computer program for analysis of imperfection sensitivity of ring stiffened shells of revolution (National Aeronautics and Space Administration ;, 1971), also by Gerald A. Cohen and Philco-Ford Corporation (page images at HathiTrust)
• Langley Research Center: A computer program for anisotropic shallow-shell finite elements using symbolic integration (U.S. National Aeronautics and Space Administration ;, 1976), also by C. M. Andersen, John T. Bowen, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Computer program for calculating flow parameters and power requirements for cryogenic wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by David A. Dress (page images at HathiTrust)
• Langley Research Center: A computer program for calculation of spectral radiative properties of gas mixtures (National Aeronautics and Space Administration ;, 1975), also by John E. Nealy (page images at HathiTrust)
• Langley Research Center: Computer program for estimating performance of air-breathing aircraft engines (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Karl A. Geiselhart, Shelby J. Morris, and Michael J. Caddy (page images at HathiTrust)
• Langley Research Center: A computer program for estimating the power-density spectrum of advanced continuous simulation language generated time histories (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by H. J. Dunn and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A computer program for fitting smooth surfaces to an aircraft configuration and other three-dimensional geometries (National Aeronautics and Space Administration, 1975), also by Charlotte B. Craidon and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Computer program for solving gains required for steady-state decoupling of elements of longitudinal mode of an airplane (National Aeronautics and Space Administration, 1974), also by G. Kimball Miller and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Computer program for supersonic kernel-function flutter analysis of thin lifting surfaces (National Aeronautics and Space Administration ;, 1974), also by Herbert J. Cunningham (page images at HathiTrust)
• Langley Research Center: A computer program for the generation of logic networks from task chart data (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Henry E. Herbert and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Computer program for thin-wire structures in a homogeneous conducting medium (National Aeronautics and Space Administration ;, 1974), also by J. H. Richmond and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: A computer program for wing subsonic aerodynamic performance estimates including attainable thrust and vortex lift effects (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Harry W. Carlson, Kenneth B. Walkley, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Computer program incorporating realistic blade motions and advanced acoustic formulations. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Kenneth S. Brentner (page images at HathiTrust)
• Langley Research Center: A computer program to calculate the longitudinal aerodynamic characteristics of wing-flap configurations with extremely blown flaps (National Aeronautics and Space Administration ;, 1976), also by M. R. Mendenhall, Selden B. Spangler, Frederick K. Goodwin, and Nielsen Engineering & Research (page images at HathiTrust)
• Langley Research Center: Computer program to calculate three-dimensional boundary layer over wings with wall mass transfer (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by J. D. McLean, J. L. Randall, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A computer program to generate equations of motion matrices, L217 (EOM). (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A computer program to predict rotor rotational noise of a stationary rotor from blade loading coefficients (U.S. National Aeronautics and Space Administration ;, 1976), also by Ramani Ramakrishnan, Robert N. Hosier, and Donald Randall (page images at HathiTrust)
• Langley Research Center: Computer science research at Langley : proceedings of a workshop held at Langley Research Center, November 2-5-, 1981 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Susan J. Voigt, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Workshop on Computer Science Research (1981 : Langley Research Center) (page images at HathiTrust)
• Langley Research Center: A computer simulation of the afterburning processes occurring within solid rocket motor plumes in the troposphere (National Aeronautics and Space Administration ;, 1976), also by Richard I. Gomberg, Roger B. Stewart, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Computer subroutines for estimation of human exposure to radiation in low Earth orbit (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Francis A. Cucinotta and John W. Wilson (page images at HathiTrust)
• Langley Research Center: Computer subroutines for the estimation of nuclear reaction effects in proton-tissue-dose calculations (U.S. National Aeronautics and Space Administration ;, 1976), also by John W. Wilson, G. S. Khandelwal, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A computer technique for detailed analysis of mission radius and maneuverability characteristics of fighter aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Willard E. Foss and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A computerized data-reduction technique for Langmuir probe analysis of electron temperature variations in the exhaust of a magnetoplasmadynamic arc (National Aeronautics and Space Administration ;, 1967), also by David R. Brooks and James M. Hoell (page images at HathiTrust)
• Langley Research Center: A computerized symbolic integration technique for development of triangular and quadrilateral composite shallow-shell finite elements (National Aeronautics and Space Administration ;, 1975), also by Carl M. Andersen and Ahmed Khairy Noor (page images at HathiTrust)
• Langley Research Center: Computing induced velocity perturbations due to a helicopter fuselage in a free stream (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by John D. Berry and Susan L. Althoff (page images at HathiTrust)
• Langley Research Center: Computing program for axial distribution of aerodynamic normal-force characteristics for axisymmetric multistage launch vehicles (National Aeronautics and Space Administration ;, 1968), also by Ragan B. Madden (page images at HathiTrust)
• Langley Research Center: Concentration measurements of an injected gas in a supersonic stream (National Aeronautics and Space Administration ;, 1967), also by Marvin G. Torrence (page images at HathiTrust)
• Langley Research Center: Concept development of a Mach 4 high-speed civil transport (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Christopher S. Domack (page images at HathiTrust)
• Langley Research Center: A concept for a fuel efficient flight planning aid for general aviation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Bela P. Collins, C. J. Wales, Andrew L. Haines, and Mitre Corporation (page images at HathiTrust)
• Langley Research Center: Conceptual design and analysis of a dynamic scale model of the space station Freedom (National Aeronautics and Space Administration, Langley Research Center, 1994), also by D. A. Davis (page images at HathiTrust)
• Langley Research Center: Conceptual design and analysis of a large antenna utilizing electrostatic membrane management (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by A. L. Brook, Martin Marietta Denver Aerospace, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Conceptual design and analysis of an infrared horizon sensor with compensation for atmospheric variability (National Aeronautics and Space Administration, 1972), also by Antony Jalink, John A. Dodgen, Richard E. Davis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A conceptual design and operational characteristics for a Mars rover for a 1979 or 1981 Viking science mission (National Aeronautics and Space Administration ;, 1974), also by Wayne L. Darnell and Vernon W. Wessel (page images at HathiTrust)
• Langley Research Center: Conceptual design of a synchronous Mars telecommunications satellite (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Deborah M. Badi (page images at HathiTrust)
• Langley Research Center: Conceptual design optimization study (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by S. J. Hollowell, R. M. Hiyama, E. R. Beeman, and North American Aircraft (Firm) (page images at HathiTrust)
• Langley Research Center: Conceptual design studies for large free-flying solar-reflector spacecraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John M. Hedgepeth, Karl Knapp, Richard K. Miller, Astro Research Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Conceptual model of turbulent flameholding for scramjet combustors (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Paul W. Huber and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Conceptual study of a turbojet/ramjet inlet (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by John P. Weidner and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Conference abstracts (NASA, 1973), also by Va.) Conference on Laser Radar Studies of the Atmosphere (5th : 1973 : Williamsburg, Optical Society of America, and American Meteorological Society. Group on Laser Atmospheric Probing (page images at HathiTrust; US access only)
• Langley Research Center: Configuration factors for exchange of radiant energy between axisymmetrical sections of cylinders, cones, and hemispheres and their bases (National Aeronautics and Space Administration, 1961), also by Albert J. Buschman and C. M. Pittman (page images at HathiTrust)
• Langley Research Center: Consideration of some aerodynamic characteristics during take-off and landing of jet airplanes (National Aeronautics and Space Administration, 1959), also by John M. Riebe (page images at HathiTrust)
• Langley Research Center: Consideration of some factors affecting low-frequency fuselage noise transmission for propeller aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by John S. Mixson and Louis A. Roussos (page images at HathiTrust)
• Langley Research Center: Considerations for the installation of honeycomb and screeens to reduce wind-tunnel turbulence (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by James Scheiman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Consolidation of fatigue and fatigue-crack-propagation data for design use (National Aeronautics and Space Administration ;, 1975), also by Richard C. Rice and Battelle Memorial Institute. Columbus Laboratories (page images at HathiTrust)
• Langley Research Center: Construction and evaluation of a nude fast-response cold-cathode ionization gage (National Aeronautics and Space Administration ;, 1966), also by Alphonsa Smith and Leonard T. Melfi (page images at HathiTrust)
• Langley Research Center: Contribution to methods for calculating the flow about thin lifting wings at transonic speeds : Analytic expressions for the far field (National Aeronautics and Space Administration ;, 1971), also by E. B. Klunker and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Control analysis of a regenerative cabin atmosphere system (National Aeronautics and Space Administration, 1971), also by Robert D. Averill, Robert Allen Smoak, and University of Virginia (page images at HathiTrust)
• Langley Research Center: Control augmented structural synthesis (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1988), also by Robert Vernon Lust and Lucien André Schmit (page images at HathiTrust)
• Langley Research Center: Control definition study for advanced vehicles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Maris Lapins, Grumman Aerospace Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Control integration concept for hypersonic cruise-turn maneuvers (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by David L. Raney and Frederick J. Lallman (page images at HathiTrust)
• Langley Research Center: Control of a large launch vehicle with limited thrust vectoring in the presence of winds (National Aeronautics and Space Administration, 1963), also by Dennis F. Collins and Homer G. Morgan (page images at HathiTrust)
• Langley Research Center: The control of carbon dioxide cryodeposits (National Aeronautics and Space Administration ;, 1973), also by Ellsworth L. Sharpe (page images at HathiTrust)
• Langley Research Center: Control-surface hinge-moment calculations for a high-aspect-ratio supercritical wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Boyd Perry and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A controls engineering approach for analyzing airplane input-output characteristics (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by P. Douglas Arbuckle (page images at HathiTrust)
• Langley Research Center: Conversion of a spacecraft designed for manned space flight to a recoverable orbiting astronomical observatory (National Aeronautics and Space Administration :, 1964), also by Windsor L. Sherman (page images at HathiTrust)
• Langley Research Center: Cornering characteristics of the main-gear tire of the space shuttle orbiter (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Robert H. Daugherty, Martha P. Robinson, and Sandy M. Stubbs (page images at HathiTrust)
• Langley Research Center: Correction of pressure data for thermal transpiration effects in pneumatic lines (National Aeronautics and Space Administration ;, 1969), also by James A. Daggerhart and North Carolina State University (page images at HathiTrust)
• Langley Research Center: Corrections to the participant-spectator model of high-energy alpha-particle fragmentation (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Francis A. Cucinotta (page images at HathiTrust)
• Langley Research Center: Correlation formulas and tables of density and some transport properties of equilibrium dissociating air for use in solutions of the boundary-layer equations (National Aeronautics and Space Administration, 1960), also by Nathaniel B. Cohen (page images at HathiTrust)
• Langley Research Center: Correlation of full-scale drag predictions with flight measurements on the C-141A aircraft : phase II, wind tunnel test, analysis, and prediction techniques (National Aeronautics and Space Administration ;, 1974), also by D. G. MacWilkinson, J. H. Paterson, W. T. Blackerby, and Lockheed-Georgia Company (page images at HathiTrust)
• Langley Research Center: Correlation of helicopter impulsive noise from blade-vortex interaction with rotor mean inflow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Andrew B. Connor and R. M. Martin (page images at HathiTrust)
• Langley Research Center: A Correlation of mixing noise from coannular jets with inverted flow profiles (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by S. Paul Pao, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Correlation of new hypervelocity impact data by threshold penetration relations (National Aeronautics and Space Administration ;, 1973), also by Robert J. Hayduk, Emilio Alfaro-Bou, Paul S. Gough, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The correlation of oblique shock parameters for ratios of specific heats from 1 to 5/3 with application to real gas flows (National Aeronautics and Space Administration, 1963), also by Mitchel H. Bertram, Barbara S. Cook, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Correlation of sonic-boom theory with wind-tunnel and flight measurements (National Aeronautics and Space Administration, 1964), also by Harry W. Carlson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Correlations for determining thermodynamic properties of hydrogen-helium gas mixtures at temperatures from 7000 to 35 000 K (U.S. National Aeronautics and Space Administration ;, 1976), also by Ernest V. Zoby, Randolph A. Graves, Peter A. Gnoffo, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A cost assessment of reliability requirements for shuttle-recoverable experiments (National Aeronautics and Space Administration ;, 1975), also by Janet W. Campbell (page images at HathiTrust)
• Langley Research Center: Coupled rotor/airframe vibration analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Robert Sopher, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, United Technologies Corporation. Sikorsky Aircraft Division, and Army Research and Technology Laboratories (U.S.). Structures Laboratory (page images at HathiTrust)
• Langley Research Center: Crack-closure and crack-growth measurements in surface-flawed titanium alloy Ti-6Al-4V (National Aeronautics and Space Administration ;, 1975), also by Elber Wolf (page images at HathiTrust)
• Langley Research Center: Crack-opening displacements in center-crack, compact, and crack-line wedge-loaded specimens (National Aeronautics and Space Administration ;, 1976), also by J. C. Newman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Crack propagation, delayed failure, and residual static strength of titanium, aluminum, and stainless steel alloys in aqueous environments (National Aeronautics and Space Administration, 1967), also by I. E. Figge and C. Michael Hudson (page images at HathiTrust)
• Langley Research Center: A cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by C. A. Bigelow (page images at HathiTrust)
• Langley Research Center: Crash simulation of vertical drop tests of two Boeing 737 fuselage sections (U.S. Federal Aviation Administration, Office of Aviation Research ;, 2002), also by Karen E. Jackson, Edwin L. Fasanella, Vehicle Technology Directorate (U.S. Army Research Laboratory), William J. Hughes Technical Center (U.S.), and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Langley Research Center: Criteria for self-ignition of supersonic hydrogen-air mixtures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Paul W. Huber, Charles R. McClinton, Charles J. Schexnayder, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Criteria for thermal regulation for manned spacecraft cabins (National Aeronautics and Space Administration ;, 1966), also by Robert W. Johnson (page images at HathiTrust)
• Langley Research Center: A critical examination of stresses in an elastic single lap joint (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Paul A. Cooper, James Wayne Sawyer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Critical requirements for the design of large space structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John M. Hedgepeth and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Critical study of higher order numerical methods for solving the boundary-layer equations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Stephen F. Wornom and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Cross section calculations for subthreshold pion production in peripheral heavy-ion collisions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by John W. Norbury (page images at HathiTrust)
• Langley Research Center: Cross-sectional deformations of monocoque beams and their side effects on the natural vibration frequencies (National Aeronautics and Space Administration, 1961), also by Robert G. Thomson, Edwin T. Kruszewski, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Cross-spectral functions based on von Karman's spectral equation (National Aeronautics and Space Administration ;, 1972), also by John C. Houbolt, Asim Sen, and Aeronautical Research Associates of Princeton (page images at HathiTrust)
• Langley Research Center: Crossflow in two-dimensional asymmetric nozzles (National Aeronautics and Space Administration ;, 1975), also by Daniel I. Sebacher and Louis P. Lee (page images at HathiTrust)
• Langley Research Center: Cryogenic performance of slotted brazed Rene ́41 honeycomb panels (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), also by Andrew K. Hepler, Allan R. Swegle, Boeing Aerospace Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Cryogenic temperature effects on sting-balance deflections in the National Transonic Facility (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Thomas G. Popernack and Jerry B. Adcock (page images at HathiTrust)
• Langley Research Center: The Cryogenic wind-tunnel concept for high Reynolds number testing (National Aeronautics and Space Administration ;, 1974), also by Robert A. Kilgore (page images at HathiTrust)
• Langley Research Center: Cryogenic wind tunnel models; design and fabrication : proceedings of a workshop held at NASA Langley Research Center, Hampton, Virginia, May 5-9, 1982 (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983), also by Blair B. Gloss, Clarence P. Young, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Cryogenic Wind Tunnel Models Workshop (1982 : NASA Langley Research Center) (page images at HathiTrust)
• Langley Research Center: Cryogenic wind tunnels : a selected, annotated bibliography (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Marie H. Tuttle, Robert A. Kilgore, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Cryogenic wind tunnels : a selected, annotated bibliography (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Marie H. Tuttle, Karen L. Cole, Robert A. Kilgore, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Cumulative annoyance due to multiple aircraft flyovers with differing peak noise levels (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Kevin P. Shepherd and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Current technology for thermal protection systems : proceedings of a workshop (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Stephen J. Scotti, Langley Research Center. Langley Thermophysics Committee, United States National Aeronautics and Space Administration, and Current Technology for Thermal Protection Systems Workshop (1992 : Langley Research Center.) (page images at HathiTrust)
• Langley Research Center: A curvature-corrected Kirchoff formulation for radar sea-return from the near vertical (National Aeronautics and Space Administration, 1974), also by Frederick C. Jackson and New York University (page images at HathiTrust)
• Langley Research Center: Curve fits of predicted inviscid stagnation-point radiative heating rates, cooling factors, and shock standoff distances for hyperbolic earth entry (National Aeronautics and Space Administration ;, 1974), also by John T. Suttles, Stephen B. Margolis, and Edward M. Sullivan (page images at HathiTrust)
• Langley Research Center: Cyclic debonding of adhesive joints : summary report (National Aeronautics and Space Administration ;, 1973), also by Daniel J. Hoffman, R. R. June, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Cyclic debonding of unidirectional composite bonded to aluminum sheet for constant-amplitiude loading (National Aeronautics and Space Administration ;, 1976), also by George L. Roderick, John H. Crews, and Richard A. Everett (page images at HathiTrust)
• Langley Research Center: Data base architecture for instrument characteristics critical to spacecraft conceptual design (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Lawrence F. Rowell and Cheryl L. Allen (page images at HathiTrust)
• Langley Research Center: Data quality : 1979 Southeastern Virginia Urban Plume Study (SEV-UPS) : surface and airborne studies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by J. H. White, Research Triangle Institute. Systems and Measurements Division, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Data quality analysis at the National Transonic Facility (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Pamela N. Stewart and Wyle Laboratories (page images at HathiTrust)
• Langley Research Center: A data reduction technique and associated computer program for obtaining vehicle attitudes with a single onboard camera (National Aeronautics and Space Administration ;, 1974), also by Richard J. Bendura and Philip G. Renfroe (page images at HathiTrust)
• Langley Research Center: Data-reduction technique for determining rapidly rising heating rates to thermally thick walls (National Aeronautics and Space Administration ;, 1969), also by James L. Dillon, G. Louis Smith, Robert L. Wright, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Davidon-Broyden rank-one minimization methods in Hilbert space with application to optimal control problems (National Aeronautics and Space Administration ;, 1972), also by Terry A. Straeter (page images at HathiTrust)
• Langley Research Center: Declination, radial distance, and phases of the moon for the years 1961 to 1971 for use in trajectory considerations (National Aeronautics and Space Administration, 1961), also by Donald S. Woolston (page images at HathiTrust)
• Langley Research Center: Deconvolution and analysis of wide-angle longwave radiation data from Nimbus 6 Earth radiation budget experiment for the first year (National Aeronautics and Space Administration, Scientific and Technical Information Branch], 1980), also by T. Dale Bess, G. Louis Smith, Richard N. Green, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Deconvolution of gas chromatographic data (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Samuel Howard, Grayson H. Rayborn, University of Southern Mississippi, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Decoupled control of a long flexible beam in orbit (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Harold A. Hamer, Katherine G. Johnson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Decoupling in linear time-varying multivariable systems (National Aeronautics and Space Administration ;, 1973), also by Viswanathan Sankaran (page images at HathiTrust)
• Langley Research Center: Deep anisotropic shell program for tire analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981), also by Carl M. Andersen, College of William and Mary, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Definition of air quality measurements for monitoring space shuttle launches (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Roger D. Thorpe (page images at HathiTrust)
• Langley Research Center: Definition of the 2005 flight deck environment (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by K. W. Alter, D. M. Regal, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: Deformation measurements of composite multi-span beam shear specimens by moire interferometry (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Daniel Post and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Delivery performance of conventional aircraft by terminal-area, time-based air traffic control : a real-time simulation evaluation (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Leonard Credeur (page images at HathiTrust)
• Langley Research Center: Demonstration of a sterilizable solid rocket motor system (National Aeronautics and Space Administration ;, 1975), also by E. J. Mastrolia, W. L. Lambert, G. M. Santerre, and Aerojet Solid Propulsion Company (page images at HathiTrust)
• Langley Research Center: Demonstration of the range over which the Langley Research Center digital computer charring ablation program (CHAP) can be used with confidence : comparisons of CHAP predictions and test data for three ablation materials (National Aeronautics and Space Administration ;, 1972), also by Carl B. Moyer, Kenneth A. Green, and Aerotherm Corporation (page images at HathiTrust)
• Langley Research Center: Dense plasma focus production in a hypocycloidal pinch (National Aeronautics and Space Administration ;, 1975), also by Ja H. Lee, Frank Hohl, and Donald R. McFarland (page images at HathiTrust)
• Langley Research Center: The density of eigenvalues in thin circular conical shells (National Aeronautics and Space Administration, 1970), also by David K. Miller and Franklin D. Hart (page images at HathiTrust)
• Langley Research Center: The dependency of penetration on the momentum per unit area of the impacting projectile and the resistance of materials to penetration (National Aeronautics and Space Administration, 1960), also by Rufus Davis Collins and William H. Kinard (page images at HathiTrust)
• Langley Research Center: Deployment and performance characteristics of 1.5-meter supersonic attached inflatable decelerators (National Aeronautics and Space Administration ;, 1974), also by Herman L. Bohon, Robert Miserentino, and James Wayne Sawyer (page images at HathiTrust)
• Langley Research Center: Deployment and performance characteristics of 5-foot-diameter (1.5 m) attached inflatable decelerators from Mach number 2.2 to 4.4 (National Aeronautics and Space Administration, 1970), also by Herman L. Bohon, Robert Miserentino, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Deployment, dynamic stability, and control characteristics of a 1/12-scale dynamic radio-controlled model of a large booster and parawing (NASA, 1963), also by Sanger M. Burk and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Deployment of a parawing recovery device for a radio-controlled 1/5-scale dynamic model spacecraft (NASA, 1963), also by Charles E. Libby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Derivation of a meteorological body of data covering the Northern Hemisphere in the longitude region between 60⁰W and 160⁰W from March 1964 through February 1965 (National Aeronautics and Space Administration, 1967), also by Roy E. Peterson, United States National Aeronautics and Space Administration, and Honeywell Inc (page images at HathiTrust)
• Langley Research Center: Derivation of approximate equations for solving the planar rendezvous problem (National Aeronautics and Space Administration ;, 1968), also by Gene W. Sparrow, Douglas B. Price, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Derivation of formulas for root-mean-square errors in location, orientation, and shape in triangulation solution of an elongated object in space (National Aeronautics and Space Administration ;, 1974), also by Sheila Ann T. Long (page images at HathiTrust)
• Langley Research Center: Derivation of transformation formulas between geocentric and geodetic coordinates for nonzero altitudes (National Aeronautics and Space Administration ;, 1974), also by Sheila Ann T. Long (page images at HathiTrust)
• Langley Research Center: Descent strategy comparisons for TNAV-equipped aircraft under airplane-preferred operating conditions (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by K. H. Izumi and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: A describing-function analysis of the stability of a launch vehicle with nonlinear thrust vectoring (National Aeronautics and Space Administration ;, 1965), also by Harold C. Lester (page images at HathiTrust)
• Langley Research Center: Description and calibration of the Langley 6- by 19-inch transonic tunnel (National Aeronautics and Space Administration ;, 1973), also by Charles L. Ladson (page images at HathiTrust)
• Langley Research Center: Description and calibration of the Langley 6- by 28-inch transonic tunnel (National Aeronautics and Space Administration ;, 1975), also by Charles L. Ladson (page images at HathiTrust)
• Langley Research Center: Description and calibration of the Langley hypersonic CF₄ tunnel : a facility for simulating low [gamma] flow as occurs for a real gas (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Raymond E. Midden and Charles G. Miller (page images at HathiTrust)
• Langley Research Center: Description and calibration of the Langley Unitary Plan Wind Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Charlie M. Jackson, William J. Monta, William A. Corlett, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Description and field test results of an in situ coliform monitoring system (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by David C. Grana, Judd Rice Wilkins, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Description and initial operating performance of the Langley 6-inch expansion tube using heated helium driver gas (National Aeronautics and Space Administration ;, 1975), also by John A. Moore (page images at HathiTrust)
• Langley Research Center: Description and operating performance of a parallel-rail electric-arc system with helium driver gas for the Langley 6-inch expansion tube (National Aeronautics and Space Administration ;, 1976), also by John A. Moore and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Description and performance of the Langley differential maneuvering simulator (National Aeronautics and Space Administration ;, 1973), also by Billy R. Ashworth, William M. Kahlbaum, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Description and performance of three Trailblazer II reentry research vehicles (National Aeronautics and Space Administration :, 1964), also by Reginald R. Lundstrom, W. Ray Hook, and Allen B. Henning (page images at HathiTrust)
• Langley Research Center: Description and preliminary studies of a computer drawn instrument landing approach display (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by James J. Adams, Frederick J. Lallman, and United States. National Aeronautics and Space Administration. Scientific and Technical Informtion Office (page images at HathiTrust)
• Langley Research Center: Description and simulation of an integrated power and attitude control system concept for space-vehicle application (National Aeronautics and Space Administration ;, 1974), also by Ralph W. Will, Kenneth L. Jacobs, and Claude R. Keckler (page images at HathiTrust)
• Langley Research Center: Description of 0.186-scale model of high-speed duct of national transonic facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Garl L. Gentry, Dennis E. Fuller, William B. Igoe, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Description of a 2-foot hypersonic facility at the Langley Research Center (National Aeronautics and Space Administration, 1961), also by George M. Stokes (page images at HathiTrust)
• Langley Research Center: Description of a computer program and numerical technique for developing linear perturbation models from nonlinear systems simulation (National Aeronautics and Space Administration :, 1978), also by James E. Dieudonne and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Description of an experimental (hydrogen peroxide) rocket system and its use in measuring aileron and rudder effectiveness of a light airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Thomas C. O'Bryan and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Description of Langley low-frequency noise facility and study of human response to noise frequencies below 50 cps (National Aeronautics and Space Administration ;, 1966), also by Philip M. Edge and William H. Mayes (page images at HathiTrust)
• Langley Research Center: Description of recent changes in the Langley 6- by 28-inch transonic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by William G. Sewall and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A description of the active and passive sidewall-boundary-layer removal systems of the 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Charles B. Johnson, Edward J. Ray, and A. V. Murthy (page images at HathiTrust)
• Langley Research Center: Description of the meteoroid detection experiment flown on the Pioneer 10 and 11 Jupiter flyby missions (National Aeronautics and Space Administration ;, 1974), also by Robert L. O'Neal (page images at HathiTrust)
• Langley Research Center: Description of the VTOL approach and landing technology (VALT) Ch-47 research system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by James R. Kelly and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Design and analysis of a rate augmented digital-to-analog converter (National Aeronautics and Space Administration ;, 1967), also by Sheldon Kopelson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Design and analysis of a star image motion compensator (National Aeronautics and Space Administration ;, 1973), also by K. C. Romanczyk, William E. Howell, and Aaron J. Ostroff (page images at HathiTrust)
• Langley Research Center: Design and analysis of a torsion braid pendulum displacement transducer (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Emanuel Rind, Emmett L. Bryant, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Design and analysis of an active jet control system for helicopter sling loads (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Mark D. Pardue, J. D. Shaughnessy, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Old Dominion University (page images at HathiTrust)
• Langley Research Center: Design and development of the spinning mode synthesizer (National Aeronautics and Space Administration ;, 1973), also by John M. Seiner, Gerhard Reethof, and Pennsylvania State University (page images at HathiTrust)
• Langley Research Center: Design and evaluation of a filter spectrometer concept for facsimile cameras (National Aeronautics and Space Administration ;, 1974), also by W. Lane Kelly, Carroll W. Rowland, and Daniel J. Jobson (page images at HathiTrust)
• Langley Research Center: Design and evaluation of active cooling systems for Mach 6 cruise vehicle wings (National Aeronautics and Space Administration ;, 1971), also by W. A. McConarty, F. M. Anthony, and Bell Aerospace Company (page images at HathiTrust)
• Langley Research Center: Design and evaluation of an optical fine-pointing control system for telescopes utilizing a digital star sensor (National Aeronautics and Space Administration ;, 1973), also by Aaron J. Ostroff and K. C. Romanczyk (page images at HathiTrust)
• Langley Research Center: Design and evaluation of controls for drift, video gain, and color balance in spaceborne facsimile cameras (National Aeronautics and Space Administration ;, 1973), also by S. J. Katzberg, Ernest E. Burcher, Carroll W. Rowland, W. Lane Kelly, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Design and experimental results for a Natural-Laminar-Flow airfoil for general aviation application (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Dan M. Somers and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Design and experimental results of a highly loaded, low solidity tandem rotor (National Aeronautics and Space Administration ;, 1971), also by James L. Bettner and General Motors Corporation (page images at HathiTrust)
• Langley Research Center: Design and fabrication of a stringer stiffened discrete tube actively cooled panel for a hypersonic aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Frank M. Anthony, Robert G. Helenbrook, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Design and fabrication of composite wing panels containing a production splice (National Aeronautics and Space Administration ;, 1975), also by D. L. Reed and General Dynamics Corporation. Fort Worth Division (page images at HathiTrust)
• Langley Research Center: Design and implementation of a telecommunication interface for the TAATM/TCV real-time experiment (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Joseph D. Nolan and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Design and implementation of robust decentralized control laws for the ACES structure at Marshall Space Flight Center (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Emmanuel G. Collins, David C. Hyland, Douglas J. Phillips, and Harris Corporation. Government Aerospace Systems Division (page images at HathiTrust)
• Langley Research Center: Design and performance at a local Mach number of 6 of an inlet for an integrated scramjet concept (National Aeronautics and Space Administration ;, 1975), also by Carl A. Trexler and Sue W. Souders (page images at HathiTrust)
• Langley Research Center: Design and performance of the University of Michigan 6.6-inch hypersonic wind tunnel (National Aeronautics and Space Administration ;, 1975), also by James L. Amick and University of Michigan (page images at HathiTrust)
• Langley Research Center: Design and preliminary tests of a blade tip air mass injection system for vortex modification and possible noise reduction on a full-scale helicopter rotor (National Aeronautics and Space Administration ;, 1975), also by Robert J. Pegg (page images at HathiTrust)
• Langley Research Center: The design and uncertainty analysis of an improved total hemispherical emittance transient calorimeter (National Aeronautics and Space Administration ;, 1969), also by William R. Wade and Donald J. Progar (page images at HathiTrust)
• Langley Research Center: A design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets (National Aeronautics and Space Administration ;, 1976), also by Richard T. Whitcomb and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A design approach to real-time formatting of high speed multispectral image data (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1981), also by Barry D. Meredith, W. Lane Kelly, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Design concepts for large reflector antenna structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by John M. Hedgepeth, Louis R. Adams, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Astro Research Corporation (page images at HathiTrust)
• Langley Research Center: Design data for brazed Rene ́41 honeycomb sandwich (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Andrew K. Hepler, Boeing Aerospace Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Design detail verification tests for a lightly loaded open-corrugation graphite-epoxy cylinder (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Randall C. Davis, James H. Starnes, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Design, development, and field testing of infrared heterodyne radiometer (IHR) for remote profiling of tropospheric and stratospheric species (National Aeronauticas and Space Administration, Scientific and Technical Information Branch ;, 1981), also by R. Lange, B. Peyton, M. Savage, Eaton Corporation. AIL Division, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Design, fabrication and systems integration of a satellite tracked, free-drifting ocean data buoy (National Aeronautics and Space Administration, Langley Research Center ;, 1976), also by John W Wallace and John W Cox (page images at HathiTrust)
• Langley Research Center: Design, fabrication and test of graphite/polyimide composite joints and attachments : summary (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by J. B. Cushman, S. F. McCleskey, S. H. Ward, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Boeing Aerospace Company. Engineering Technology (page images at HathiTrust)
• Langley Research Center: Design, implementation and flight testing of PIF autopilots for general aviation aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by John R. Broussard and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Design of a convective cooling system for a Mach 6 hypersonic transport airframe (National Aeronautics and Space Administration ;, 1971), also by R. G. Helenbrook, F. M. Anthony, and Bell Aerospace Company (page images at HathiTrust)
• Langley Research Center: The Design of aircraft using the decision support problem technique (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Farokh Mistree (page images at HathiTrust)
• Langley Research Center: Design of an electronically scanned star sensor with digital output (National Aeronautics and Space Administration ;, 1969), also by Aaron J. Ostroff, K. C. Romanczyk, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Design of bodies to produce specified sonic-boom signatures (National Aeronautics and Space Administration, 1968), also by Raymond L. Barger and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Design of integrated pitch axis for autopilot/autothrottle and integrated lateral axis for autopilot/yaw damper for NASA TSRV airplane using integral LQG methodology (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Isaac Kaminer and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Design of microstrip components by computer (National Aeronautics and Space Administration ;, 1972), also by Terry C. Cisco and CAED Corporation (page images at HathiTrust)
• Langley Research Center: Design of passive piezoelectric damping for space structures (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Nesbitt W. Hagood, Andreas H. von Flotow, and Jack B. Aldrich (page images at HathiTrust)
• Langley Research Center: The design of sailplanes for optimum thermal soaring performance (National Aeronautics and Space Administration, 1964), also by Clarence D. Cone and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Design of the Annular Suspension and Pointing System (ASPS) : (including design addendum) (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by D. Cunningham and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Design optimization of natural laminar flow bodies in compressible flow (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), also by Simha S. Dodbele and Inc ViGYAN (page images at HathiTrust)
• Langley Research Center: Design, performance, and calculated error of a Faraday cup for absolute beam current measurements of 600-MeV protons (National Aeronautics and Space Administration ;, 1975), also by Sherwin M. Beck (page images at HathiTrust)
• Langley Research Center: A design procedure for a tension-wire stiffened truss-column (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by William H. Greene and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A Design study for a simple-to-fly, constant attitude light aircraft (National Aeronautics and Space Administration ;, 1973), also by Frederick O. Smetana and North Carolina State University (page images at HathiTrust)
• Langley Research Center: Design study of software-implemented fault-tolerance (SIFT) computer (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), also by J. H. Wensley, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and SRI International (page images at HathiTrust)
• Langley Research Center: A design summary of stall characteristics of straight wing aircraft (National Aeronautics and Space Administration ;, 1971), also by M. A. McVeigh, E. Kisielowski, United States National Aeronautics and Space Administration, and Dynasciences Corporation. Scientific Systems Division (page images at HathiTrust)
• Langley Research Center: Design trends for Army/Air Force airplanes in the United States (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by M. Leroy Spearman (page images at HathiTrust)
• Langley Research Center: Detailed design of a ride quality augmentation system for commuter aircraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Reiner Suikat, David R. Downing, and Kent E. Donaldson (page images at HathiTrust)
• Langley Research Center: Detailed flow-field measurements over a 75 ̊swept delta wing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Scott O. Kjelgaard and William L. Sellers (page images at HathiTrust)
• Langley Research Center: Detailed pressure distribution measurements obtained on several configurations of an aspect-ratio-7 variable twist wing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by G. Thomas Holbrook and Dana Morris Dunham (page images at HathiTrust)
• Langley Research Center: Determination of airplane model structure from flight data by using modified stepwise regression / /c Vladislav Klein, James G. Batterson and Patrick C. Murphy. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Vladislav Klein, Patrick C. Murphy, James G. Batterson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Determination of corrections to flow direction sensor measurements over an angle-of-attack range from 0 ̊to 85 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Thomas M. Moul (page images at HathiTrust)
• Langley Research Center: Determination of depth-viewing volumes for stereo three-dimensional graphic displays (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Russell V. Parrish, Steven P. Williams, United States. Army Aviation Systems Command, and United States. Army Aviation Research and Development Command (page images at HathiTrust)
• Langley Research Center: Determination of effects of oxidation on performance of charring ablators (National Aeronautics and Space Administration [For sale by the Office of Technical Services, Dept. of Commerce, Washington, D.C. 20230], 1964), also by Marvin B. Dow, Robert T. Swann, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Determination of flight characteristics of supersonic transports during the landing approach with a large jet transport in-flight simulator (National Aeronautics and Space Administration, 1967), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Determination of flight hardware configuration of energy-absorbing attenuator for proposed space station crew and equipment translation aid cart (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Edwin L. Fasanella and United States. Army. Aerostructures Directorate (page images at HathiTrust)
• Langley Research Center: Determination of lunar equatorial radius using image-motion compensation sensor data from Lunar Orbiter I (National Aeronautics and Space Administration ;, 1969), also by Harold R. Compton, William R. Wells, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Determination of mean atmospheric densities during minimum solar activity by means of the Explorer XIX satellite (National Aeronautics and Space Administration, 1966), also by James A. Mullins and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Determination of rotor harmonic blade loads from acoustic measurements (National Aeronautics and Space Administration ;, 1975), also by Peter K. Kasper, U.S. Army Air Mobility Research and Development Laboratory, and Wyle Laboratories (page images at HathiTrust)
• Langley Research Center: Determination of the hypersonic-continuum/rarefield-flow drag coefficient of the Viking Lander Capsule 1 aeroshell from flight data (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Robert C. Blanchard, Gerald D. Walberg, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Development and application of a gradient method for solving differential games (National Aeronautics and Space Administration ;, 1971), also by David A. Roberts, Raymond C. Montgomery, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Development and application of a local linearization algorithm for the integration of quaternion rate equations in real-time flight simulation problems (National Aeronautics and Space Administration ;, 1973), also by Lawrence E. Barker, Louise H. Williams, Roland L. Bowles, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Development and application of a method for predicting rotor free wake positions and resulting rotor blade air loads. Volume 1, Model and results (National Aeronautics and Space Administration ;, 1971), also by S. G. Sadler and Rochester Applied Sciences Associates (page images at HathiTrust)
• Langley Research Center: Development and application of a method for predicting rotor free wake positions and resulting rotor blade air loads. Volume 2, Program listings (National Aeronautics and Space Administration ;, 1971), also by S. G. Sadler and Rochester Applied Sciences Associates (page images at HathiTrust)
• Langley Research Center: Development and application of a photoelasto-plastic method to study stress distributions in vicinity of a simulated crack (National Aeronautics and Space Administration] ;, 1966), also by A. R. Hunter, M. E. Schwarz, Lockheed Aircraft Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Development and application of the GIM code for the CYBER 203 computer (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by J. F. Stalnaker, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Langley Research Center: Development and applications of supersonic unsteady consistent aerodynamics for interfering parallel wings (National Aeronautics and Space Administration ;, 1973), also by Kari Appa, G. C. C. Smith, and Bell Aerospace Company (page images at HathiTrust)
• Langley Research Center: Development and applications of two computational procedures for determining the vibration modes of structural systems (National Aeronautics and Space Administration ;, 1975), also by Raymond G. Kvaternik (page images at HathiTrust)
• Langley Research Center: Development and demonstration of a flutter-suppression system using active controls (National Aeronautics and Space Administration ;, 1975), also by M. C. Sandford, David L. Gray, and Irving Abel (page images at HathiTrust)
• Langley Research Center: Development and demonstration of flueric sounding rocket motor ignition (National Aeronautics and Space Administration ;, 1974), also by Vincent P. Marchese and Singer Company. Kearfott Division (page images at HathiTrust)
• Langley Research Center: Development and evaluation of an airplane electronic display format aligned with the inertial velocity vector (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by George G. Steinmetz (page images at HathiTrust)
• Langley Research Center: Development and evaluation of vacuum pressure gauge components from carbon and graphite (National Aeronautics and Space Administration ;, 1972), also by David K. Benson, George A. Beitel, and Mo.) Midwest Research Institute (Kansas City (page images at HathiTrust)
• Langley Research Center: Development and flight test of the Multichannel Ocean Colar Sensor (MOCS) (National Aeronautics and Space Administration ;, 1973), also by P. G. White and TRW Systems Group (page images at HathiTrust)
• Langley Research Center: Development and flight tests of a gyro-less wing leveler and directional autopilot (National Aeronautics and Space Administration ;, 1974), also by H. Douglas Garner and Harold E. Poole (page images at HathiTrust)
• Langley Research Center: The Development and preliminary application of an invariant coupled diffusion and chemistry model (National Aeronautics and Space Administration ;, 1973), also by Glenn R. Hilst and Aeronautical Research Associates of Princeton (page images at HathiTrust)
• Langley Research Center: Development and test results of a flight management algorithm for fuel-conservation descents in a time-based metered traffic environment (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Charles E. Knox, Dennis G. Cannon, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Development and testing of a proposed infrared horizon scanner for use in spacecraft attitude determination (National Aeronautics and Space Administration ;, 1965), also by Norman M. Hatcher, Nelson J. Groom, and Arthur L. Newcomb (page images at HathiTrust)
• Langley Research Center: Development and testing of cabin sidewall acoustic resonators for the reduction of cabin tone levels in propfan-powered aircraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by H. L. Kuntz and Lockheed Aeronautical Systems Company (page images at HathiTrust)
• Langley Research Center: Development and validation of a combined rotor-fuselage induced flow-field computational method (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Carl E. Freeman, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Development and validation of a piloted simulation of a helicopter and external sling load (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by J. D. Shaughnessy, Kenneth R. Yenni, Thomas N. Deaux, Sperry Support Services, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Development and validation of cryogenic foam insulation for LH₂ subsonic transports (National Aeronautics and Space Administration Branch ;, 1981), also by Frank M. Anthony, R. G. Helenbrook, J. Z. Colt, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Development, fabrication, and testing of a magnetically connected plastic vacuum probe surface sampler (National Aeronautics and Space Administration ;, 1972), also by G. Briggs Phillips, V. A. Pace, and Becton Dickinson Research Center (page images at HathiTrust)
• Langley Research Center: Development of a barium chemical release system (National Aeronautics and Space Administration ;, 1969), also by C. S. Stokes, W. J. Murphy, E. W. Smith, and Temple University (page images at HathiTrust)
• Langley Research Center: Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume II - code description (U.S. National Aeronautics and Space Administration ;, 1976), also by Frank Marconi, Larry Yaeger, United States National Aeronautics and Space Administration, and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Development of a computer program to obtain ordinates for NACA 4-digit, 4-digit modified, 5-digit, and 16-series airfoils (National Aeronautics and Space Administration ;, 1975), also by Charles L. Ladson and Cuyler W. Brooks (page images at HathiTrust)
• Langley Research Center: Development of a computer program to obtain ordinates from NACA 6- and 6A-series airfoils (National Aeronautics and Space Administration ;, 1974), also by Charles L. Ladson and Cuyler W. Brooks (page images at HathiTrust)
• Langley Research Center: Development of a digital guidance and control law for steep approach automatic landings using modern control techniques (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Nesim Halyo and Analytical Mechanics Associates (page images at HathiTrust)
• Langley Research Center: Development of a Fowler flap system for a high performance general aviation airfoil (National Aeronautics and Space Administration ;, 1974), also by W. H. Wentz, H. C. Seetharam, University of Kansas. Center for Research, and Wichita State University (page images at HathiTrust)
• Langley Research Center: Development of a machine vision system for automated structural assembly (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by P. Daniel Sydow and Eric G. Cooper (page images at HathiTrust)
• Langley Research Center: Development of a monolithic ferrite memory array (National Aeronautics and Space Administration ;, 1972), also by C. H. Heckler, N. C. Bhiwandker, and Ampex Corporation (page images at HathiTrust)
• Langley Research Center: Development of a near-wall Reynolds-stress closure based on the SSG model for the pressure strain (National Aeronautics and Space Administration, Langley Research Center, 1994), also by R. M. C. So (page images at HathiTrust)
• Langley Research Center: Development of a noise annoyance sensitivity scale (National Aeronautics and Space Administration ;, 1972), also by Howard Louis Bregman, Richard G. Pearson, United States National Aeronautics and Space Administration, and North Carolina State University (page images at HathiTrust)
• Langley Research Center: Development of a nonlinear switching function and its application to static lift characteristics of straight wings (National Aeronautics and Space Administration, Scientific and Technical Information Service ;, 1978), also by Donald E. Hewes and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Development of a nonlinear unsteady transonic flow theory (National Aeronautics and Space Administration ;, 1973), also by Stephen S. Stahara, John R. Spreiter, and Nielsen Engineering & Research (page images at HathiTrust)
• Langley Research Center: Development of a smoke-trail vehicle for application to wind-shear measurements up to 80,000 feet (National Aeronautics and Space Administration, 1963), also by Wade E. Lanford (page images at HathiTrust)
• Langley Research Center: The development of a sonic boom simulator with detonable gases (National Aeronautics and Space Administration, 1971), also by R. T. Strugielski, United States National Aeronautics and Space Administration, and General American Research Division (page images at HathiTrust)
• Langley Research Center: Development of a sorber trace contaminant control system including pre- and post-sorbers for a catalytic oxidizer (National Aeronautics and Space Administration ;, 1972), also by Thomas M. Olcott and Lockheed Missiles and Space Company (page images at HathiTrust)
• Langley Research Center: Development of a standardized battery of performance tests for the assessment of noise stress effects (National Aeronautics and Space Administration ;, 1973), also by George C. Theologus and American Institutes for Research (page images at HathiTrust)
• Langley Research Center: Development of a superconductor magnetic suspension and balance prototype facility for studying the feasibility of applying this technique to large scale aerodynamic testing (National Aeronautics and Space Administration ;, 1975), also by R. N. Zapata, Karl C. Henderson, Robert R. Humphris, and University of Virginia. Research Laboratories for the Engineering Sciences (page images at HathiTrust)
• Langley Research Center: The development of a three-dimensional partially elliptic flow computer program for combustor research (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Y. S. Pan, Pittsburgh Energy Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Development of advanced avionics systems applicable to terminal-configured vehicles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by R. L. Heimbold, M. F. Leffler, H. P. Lee, and Lockheed-California Company (page images at HathiTrust)
• Langley Research Center: Development of aerodynamic prediction methods for irregular planform wings (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by David B. Benepe, General Dynamics Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Development of an adaptive failure-detection and identification system for detecting aircraft control-element failures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by W. Thomas Bundick (page images at HathiTrust)
• Langley Research Center: Development of an air ground data exchange concept : flight deck perspective (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987), also by G. W. Flathers and Mitre Corporation (page images at HathiTrust)
• Langley Research Center: Development of an analysis for the determination of coupled helicopter rotor/control system dynamic response (National Aeronautics and Space Administration ;, 1975), also by Lawrence R. Sutton, Stephen A. Rinehart, and Rochester Applied Sciences Associates (page images at HathiTrust)
• Langley Research Center: Development of an apparatus to measure thermophysical properties of wind tunnel heat transfer models (National Aeronautics and Space Administration ;, 1974), also by Richard F. Romanowski, Ira H. Steinberg, and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Development of an efficient procedure for calculating the aerodynamic effects of planform variation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by J. E. Mercer, E. W. Geller, Flow Research Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Development of an experiment for visible radiation polarization measurements from a satellite (National Aeronautics and Space Administration ;, 1973), also by Zdenek Sekera, Richard E. Bradbury, and Los Angeles. Institute of Geophysics and Planetary Physics University of California (page images at HathiTrust)
• Langley Research Center: Development of an optimal automatic control law and filter algorithm for steep glideslope capture and glideslope tracking (U.S. National Aeronautics and Space Administration ;, 1976), also by Nesim Halyo, United States National Aeronautics and Space Administration, and University of Virginia (page images at HathiTrust)
• Langley Research Center: Development of assembly and joint concepts for erectable space structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by G. G. Jacquemin and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Development of impedance simulation fixtures for spacecraft vibration tests (National Aeronautics and Space Administration ;, 1969), also by Terry D. Scharton and Beranek Bolt (page images at HathiTrust)
• Langley Research Center: Development of integrated programs for aerospace-vehicle design (IPAD), product manufacture interactions with the design process (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Harold A. Crowell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Development of integrated programs for aerospace-vehicle design (IPAD), product program management systems (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by J. M. Isenberg, J. W. Southall, Boeing Commercial Airplane Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Development of Integrated Programs for Aerospace-Vehicle Design (IPAD) : reference design process (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Donald D. Meyer and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Development of lasers optimized for pumping Ti:Al₂O₃ lasers (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Glen A. Rines and Richard A. Schwarz (page images at HathiTrust)
• Langley Research Center: Development of lightweight aluminum compression panels reinforced by boron-epoxy infiltrated extrusions (National Aeronautics and Space Administration ;, 1973), also by Paul A. Roy, Jim Henshaw, John A. McElman, and Avco Corporation. Systems Division (page images at HathiTrust)
• Langley Research Center: Development of low-frequency kernel-function aerodynamics for comparison with time-dependent finite-difference methods (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), also by Samuel R. Bland and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Development of new addition-type composite resins (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by R. J. Kray, CIBA-GEIGY Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Development of panel methods for subsonic analysis and design (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by D. R. Bristow and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Development of Pyrrone structural forms for honeycomb filler (National Aeronautics and Space Administration ;, 1973), also by B. G. Kimmel and Hughes Aircraft Company (page images at HathiTrust)
• Langley Research Center: Development of quality assurance methods for epoxy graphite prepreg (National Aeronautics and Space Adminstration, Scientific and Technical Information Branch ;, 1982), also by J. S. Chen, A. B. Hunter, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: The development of radiation resistant insulating layers for planar silicon technology (National Aeronautics and Space Administration ;, 1970), also by R. P. Donovan, L. K. Monteith, M. Simons, and Research Triangle Institute (page images at HathiTrust)
• Langley Research Center: Development of skylab experiment to20 employing a foot-controlled maneuvring unit (National Aeronautics and Space Administration, 1972), also by Donald E. Hewes, Kenneth E. Glover, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Development of sonic-boom signatures in a stratified atmosphere (National Aeronautics and Space Administration, 1968), also by Raymond L. Barger and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: Development of the 15 meter diameter hoop column antenna : a final report (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986), also by Harris Corporation (page images at HathiTrust)
• Langley Research Center: Development of the CSI phase-3 evolutionary model testbed (National Aeronautics and Space Administration, Langley Research Center, 1994), also by M. J. Gronet, M. K. Tan, and D. A. Davis (page images at HathiTrust)
• Langley Research Center: Development of the general interpolants method for the CYBER 200 series of supercomputers (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by J. F. Stalnaker (page images at HathiTrust)
• Langley Research Center: Development of the reentry flight dynamics simulator for evaluation of space shuttle orbiter entry systems (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Lawrence F. Rowell, Howard W. Stone, Richard W. Powell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Development of the triplet singularity for the analysis of wings and bodies in supersonic flow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by F. A. Woodward, Inc Analytical Methods, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Development of the weld-braze joining process (National Aeronautics and Space Administration ;, 1973), also by Thomas T. Bales, Winfrey E. Arnold, and Dick M. Royster (page images at HathiTrust)
• Langley Research Center: Development of tough, moisture resistant laminating resins (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by R. A. Brand, E. S. Harrison, General Dynamics Corporation. Convair Division, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Development of tunable high pressure CO2 laser for lidar measurements of pollutants and wind velocities - October 1977 through January 1979 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Jeffry S. Levine, Ali Javan, Michael Guerra, Laser Development Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Development of tunable high pressure CO2 laser for lidar measurements of pollutants and wind velocities, January 1976 to December 1977 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Ali Javan and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Development of upwind schemes for the Euler equations (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987), also by Sukumar R. Chakravarthy (page images at HathiTrust)
• Langley Research Center: A diagnostic model for studying daytime urban air-quality trends (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Dana A. Brewer, Gerard E. Woodbury, Ellis E. Remsberg, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Differential absorption and scattering sensitivity predictions (National Aeronautics and Space Administration ;, 1976), also by Richard T. Thompson, United States National Aeronautics and Space Administration, and Old Dominion University. Dept. of Physics and Geophysical Sciences (page images at HathiTrust)
• Langley Research Center: Diffracted and head waves associated with waves on nonseparable surfaces (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Raymond L. Barger (page images at HathiTrust)
• Langley Research Center: Diffraction by a perfectly conducting rectangular cylinder which is illuminated by an array of line sources (National Aeronautics and Space Administration ;, 1974), also by R. G. Kouyoumjian, N. Wang, and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: Diffusion and phase change characterization by mass spectrometry (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1979), also by Mark E. Koslin, Frederick Andrew White, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Diffusion with chemical reaction : an attempt to explain number density anomalies in experiments involving alkali vapor (National Aeronautics and Space Administration ;, 1974), also by W. L. Snow (page images at HathiTrust)
• Langley Research Center: Digital adaptive flight controller development (National Aeronautics and Space Administration ;, 1974), also by Howard Kaufman and Rensselaer Polytechnic Institute. Systems Engineering Division (page images at HathiTrust)
• Langley Research Center: Digital computer programs for generating oblique orthographic projections and contour plots (National Aeronautics and Space Administration ;, 1975), also by Gary L. Giles (page images at HathiTrust)
• Langley Research Center: A digital computer study of the buckling of shallow spherical caps and truncated hemispheres (National Aeronautics and Space Administration ;, 1972), also by William C. Stilwell, Robert E. Ball, and Naval Postgraduate School (U.S.) (page images at HathiTrust)
• Langley Research Center: Digital enhancement of flow field images (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Robert A. Kudlinski and Stephen Keith Park (page images at HathiTrust)
• Langley Research Center: Digital flight control research (National Aeronautics and Space Administration, 1974), also by James E. Potter and Massachusetts Institute of Technology. Measurement Systems Laboratory (page images at HathiTrust)
• Langley Research Center: A digitally controlled very high frequency synthesizer (National Aeronautics and Space Administration ;, 1971), also by Joan H. Middleton and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Diode laser satellite systems for beamed power transmission (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by M. D. Williams (page images at HathiTrust)
• Langley Research Center: Direct and large-eddy simulations of three-dimensional compressible Navier-Stokes turbulence (Washington, D. C. : Naval Research Laboratory, Center for Computational Physics Developments, Laboratory for Computational Physics and Fluid Dynamics Division, 1991., 1991), also by Thomas A. Zang, J. P. Dahlburg, R. B. Dahlburg, and Naval Research Laboratory (U.S.) (page images at HathiTrust)
• Langley Research Center: Direct computation of orbital sunrise or sunset event parameters (Langley Research Center, 1986), also by James J. Buglia and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A direct-inverse method for transonic and separated flows about airfoils (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Leland A. Carlson and Texas A & M University. Aerospace Engineering Dept (page images at HathiTrust)
• Langley Research Center: Direct measurement and analysis of skin friction and cooling downstream of multiple flush-slot injection into a turbulent Mach 6 boundary layer (National Aeronautics and Space Administration, Scientific and Technical Information Office :, 1978), also by Floyd G. Howard and Andrew J. Srokowski (page images at HathiTrust)
• Langley Research Center: Direct simulation of high-speed mixing layers (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by H. S. Mukunda (page images at HathiTrust)
• Langley Research Center: Directivity and trends of noise generated by a propeller in a wake (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by P. J. W. Block and Garl L. Gentry (page images at HathiTrust)
• Langley Research Center: Discomfort criteria for single-axis vibrations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Thomas K. Dempsey, Sherman A. Clevenson, Jack D. Leatherwood, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Discontinuity stresses in metallic pressure vessels. (National Aeronautics and Space Administration;, 1971), also by F. L. Rish, L. Kovalevsky, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Discrete sonic jets used as boundary-layer trips at Mach numbers of 6 and 8.5 (National Aeronautics and Space Administration ;, 1972), also by David R. Stone, Aubrey M. Cary, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Discrete-vortex model for the symmetric-vortex flow on cones (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Thomas G. Gainer (page images at HathiTrust)
• Langley Research Center: Ditching investigation of a 1/20-scale model of the space shuttle orbiter (National Aeronautics and Space Administration ;, 1975), also by William L. Thomas and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Domestic wash water reclamation for reuse as commode water supply using a filtration--reverse-osmosis separation technique (National Aeronautics and Space Administration ;, 1974), also by John B. Hall, Judd Rice Wilkins, and Carmen E. Batten (page images at HathiTrust)
• Langley Research Center: Dose response functions in the atmosphere due to incident high-energy protons, with application to solar proton events (National Aeronautics and Space Administration; [for sale by the Clearinghouse For Federal Scientific and Technical Information, Springfield, Va.], 1970), also by John William Wilson (page images at HathiTrust)
• Langley Research Center: Doubly differential cross sections for galactic heavy-ion fragmentation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Francis A. Cucinotta (page images at HathiTrust)
• Langley Research Center: Downstream influence of swept slot injection in hypersonic turbulent flow (National Aeronautics and Space Administration ;, 1977), also by Jerry N. Hefner, Dennis M. Bushnell, Aubrey M. Carey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Drag and stability characteristics of a variety of reefed and unreefed parachute configurations at Mach 1.80 with an empirical correlation for supersonic Mach numbers (National Aeronautics and Space Administration ;, 1975), also by Lana M. Couch (page images at HathiTrust)
• Langley Research Center: The drag coefficient of parabolic bodies of revolution operating at zero cavitation number and zero angle of yaw (U.S. G.P.O., 1961), also by Virgil E. Johnson, Thomas A. Rasnick, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Drag coefficients for spheres in free molecular flow in O at satellite velocities (National Aeronautics and Space Administration ;, 1973), also by John W. Boring, Robert R. Humphris, and University of Virginia (page images at HathiTrust)
• Langley Research Center: Drag measurements of blunt stores tangentially mounted on a flat plate at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Floyd J. Wilcox (page images at HathiTrust)
• Langley Research Center: Drag of a supercritical body of revolution in free flight at transonic speeds and comparison with wind-tunnel data (National Aeronautics and Space Administration ;, 1971), also by J. W. Usry, John W. Wallace, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Drop size distributions and related properties of fog for five locations measured from aircraft (National Aeronautics and Space Administration, Langley Research Center, 1994), also by J. Allen Zak (page images at HathiTrust)
• Langley Research Center: Dual methods and approximation concepts in structural synthesis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Claude Fleury, Lucien André Schmit, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: The dyadic diffraction coefficient for a curved edge (National Aeronautics and Space Administration ;, 1974), also by R. G. Kouyoumjian, P. H. Pathak, and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: DYCAST, a finite element program for the crash analysis of structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987), also by A. Pifko, P. L. Ogilvie, R. Winter, Grumman Aerospace Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: DYLOFLEX modifications to FLEXSTAB. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Patrick D'Auria and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Dynamic analysis of a simple reentry maneuver for a lifting satellite (National Aeronautics and Space Administration, 1959), also by Frederick C. Grant (page images at HathiTrust)
• Langley Research Center: Dynamic and static wind-tunnel tests of a flow-direction vane (National Aeronautics and Space Administration ;, 1971), also by Norman R. Richardson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Dynamic characteristics of a two-stage variable-mass flexible missile with internal flow (National Aeronautics and Space Administration ;, 1972), also by Leonard Meirovitch, John Bankovskis, and University of Cincinnati (page images at HathiTrust)
• Langley Research Center: Dynamic ground-effect measurements on F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Guy T. Kemmerly (page images at HathiTrust)
• Langley Research Center: Dynamic heave-pitch analysis of air cushion landing systems (National Aeronautics and Space Administration ;, 1975), also by K. M. Captain, D. N. Wormley, Ashok B. Boghani, and Foster-Miller Associates (page images at HathiTrust)
• Langley Research Center: Dynamic measurement of total temperature, pressure, and velocity in the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Charles B. Johnson and P. Calvin Stainback (page images at HathiTrust)
• Langley Research Center: A dynamic model investigation of the effect of a sharp-edge vertical gust on blade periodic flapping angles and bending moments of a two-blade rotor (National Aeronautics and Space Administration, 1959), also by John Locke McCarty, Domenic J. Maglieri, and George W. Brooks (page images at HathiTrust)
• Langley Research Center: Dynamic model investigation of touchdown stability of lunar-landing vehicles (National Aeronautics and Space Administration ;, 1967), also by Robert W. Herr and H. Wayne Leonard (page images at HathiTrust)
• Langley Research Center: Dynamic response of a forward-swept-wing model at angles of attack up to 15 at a Mach number of 0.8 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Robert V. Doggett, Rodney H. Ricketts, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Dynamic response of airplanes to atmospheric turbulence including flight data on input and response (National Aeronautics and Space Administration, 1964), also by John C. Houbolt, Kermit G. Pratt, and Roy Steiner (page images at HathiTrust)
• Langley Research Center: Dynamic response of rising and falling balloon wind sensors with application to estimates of wind loads on launch vehicles (National Aeronautics and Space Administration, 1963), also by Wilmer H. Reed and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Dynamic response of some tentative compliant wall structures to convected trubulence fields (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by H. H. Nijim, Y. K. Lin, University of Illinois at Urbana-Champaign, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Dynamic response of structural elements eposed to sonic booms (National Aeronautics and Space Administration] ;, 1969), also by David H. Cheng, City University of New York. City College, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Dynamic responses of railroad car models to vertical and lateral rail inputs (National Aeronautics and Space Administration ;, 1971), also by John L. Sewall, Barbara J. Durling, Russell V. Parrish, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Dynamic stability and dispersion of a Project Mercury test capsule upon entering the atmosphere, with effects of roll rate, center-of-gravity displacement, and threshold of a rate-reaction control system (National Aeronautics and Space Administration, 1961), also by Byron M. Jaquet and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Dynamic stability derivatives of a jet transport configuration with high thrust-weight ratio and an externally blown jet flap (National Aeronautics and Space Administration ;, 1971), also by Sue B. Grafton, Charles C. Smith, Lysle P. Parlett, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Dynamic stability derivatives of space shuttle orbiter from wind-tunnel and approach and landing flight tests (National Aeronautics and Space Administration , Scientific and Technical Information Office ;, 1980), also by Delma C. Freeman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Dynamic testing of a two-dimensional box truss beam (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987), also by Charles W. White (page images at HathiTrust)
• Langley Research Center: Dynamics of a one-dimensional plasma sheath (National Aeronautics and Space Administration ;, 1968), also by Frank Hohl, Leo D. Staton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Dynamics of aircraft antiskid braking systems (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by John A. Tanner and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Dynamics of two slowly rotating point-mass vehicles connected by a massless tether and in a circular orbit (National Aeronautics and Space Administration ;, 1970), also by William M. Adams and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Earth radiation budget science, 1978 : proceedings of a workshop (NASA, Scientific and Technical Branch ;, 1979), also by Va.) Workshop on Earth Radiation Budget Science (1978 : Williamsburg and Colorado State University (page images at HathiTrust)
• Langley Research Center: Earth radiation science seminars : lectures from a series of seminars held at Langley Research Center, Hampton, Virginia, June 1980 to October 1981 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by John B. Hall and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: The Echo I inflation system (National Aeronautics and Space Administration :, 1964), also by Dewey L. Clemmons (page images at HathiTrust)
• Langley Research Center: An economic and performance design study of solar preheaters for domestic hot water heaters in North Carolina (National Aeronautics and Space Administration ;, 1977), also by Clay B. Jones, Fredrick O. Smetana, North Carolina State University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Economic evaluation of flying-qualities design criteria for a transport configured with relaxed static stability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Steven M. Sliwa and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Edge diffracted caustic fields (National Aeronautics and Space Administration ;, 1974), also by Walter D. Burnside, L. Peters, and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: Effect of a finite ionization rate on the radiative heating of outer planet atmospheric entry probes (National Aeronauticas and Space Administration, Scientific and Technical Information Office ;, 1982), also by H. F. Nelson, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and University of Missouri--Rolla. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• Langley Research Center: Effect of a surface-to-gap temperature discontinuity on the heat transfer to reusable surface insulation tile gaps (National Aeronautics and Space Administration ;, 1976), also by David Throckmorton and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by George T. Carson, James R. Burley, and E. Ann Bare (page images at HathiTrust)
• Langley Research Center: Effect of a variable-geometry diffuser on the operating characteristics of a helium tunnel designed for a mach number in excess of 20 (National Aeronautics and Space Administration, 1960), also by Patrick J. Johnston and Robert D. Witcofski (page images at HathiTrust)
• Langley Research Center: Effect of aerodynamic and angle-of-attack uncertainties on the May 1979 entry flight control system of the space shuttle from Mach 8 to 1.5 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Howard W. Stone, Richard W. Powell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effect of aerodynamic heating on the flutter of a rectangular wing at a mach number of 2 (National Aeronautics and Space Administration :, 1960), also by Harry L. Runyan and Nan H. Jones (page images at HathiTrust)
• Langley Research Center: Effect of aileron deflections on the aerodynamic characteristics of a semispan model of a subsonic energy-efficient transport (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Peter F. Jacobs (page images at HathiTrust)
• Langley Research Center: Effect of air contamination in a helium tunnel (National Aeronautics and Space Administration, 1960), also by Arthur Henderson and Frank E. Swalley (page images at HathiTrust)
• Langley Research Center: Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing (National Aeronautics and Space Administration, Scientific and Technical Information Association ;, 1978), also by Lawrence C. Montoya, Peter F. Jacobs, Stuart G. Flechner, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: The effect of angle of attack on the buckling of Mars entry aeroshells (National Aeronautics and Space Administration ;, 1973), also by Gerald A. Cohen and Structures Research Associates (page images at HathiTrust)
• Langley Research Center: Effect of blockage ratio on drag and pressure distributions for bodies of revolution at transonic speeds (National Aeronautics and Space Administration ;, 1973), also by Lana M. Couch, Cuyler W. Brooks, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration (National Aeronautics and Space Administration :, 1978), also by Blair B. Gloss and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: The effect of canard and vertical tails on the aerodynamic characteristics of a model with a 59 ̊sweptback wing at a Mach number of 0.30 (National Aeronautics and Space Administration ;, 1974), also by William P. Henderson (page images at HathiTrust)
• Langley Research Center: Effect of canard leading-edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristics of a close-coupled canard-wing configuration (National Aeronautics and Space Administration ;, 1974), also by Blair B. Gloss (page images at HathiTrust)
• Langley Research Center: Effect of canard location and size on canard-wing interference and aerodynamic-center shift related to maneuvering aircraft at transonic speeds (National Aeronautics and Space Administration ;, 1974), also by Blair B. Gloss (page images at HathiTrust)
• Langley Research Center: Effect of canard vertical location, size, and deflection on canard-wing interference at subsonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Blair B. Gloss, Karen E. Washburn, Edward J. Ray, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Effect of chordwise heat conduction on the torsional stiffness of a diamond-shaped wing subjected to a constant heat input (National Aeronautics and Space Administration, 1959), also by Robert G. Thomson and J. Lyell Sanders (page images at HathiTrust)
• Langley Research Center: Effect of collector configuration on test section turbulence levels in an open-jet wind tunnel (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by G. S. Manuel, P. S. Barna, and John K. Molloy (page images at HathiTrust)
• Langley Research Center: Effect of concentration dependence of the diffusion coefficient on homogenization kinetics in multiphase binary alloy systems (National Aeronautics and Space Administration, Scientific and Technical Information Office :, 1978), also by Darrel R. Tenney, Jalaiah Unnam, Joint Institute for Advancement of Flight Sciences, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: The effect of configuration on strength, durability, and handle of Kevlar fabric-based materials (National Aeronautics and Space Administration ;, 1977), also by L. L. Rueter, J. B. Munson, Inc Sheldahl, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of crash pulse shape on seat stroke requirements for limiting loads on occupants of aircraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Huey D. Carden (page images at HathiTrust)
• Langley Research Center: Effect of debond growth on stress-intensity factors in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by C. A. Bigelow (page images at HathiTrust)
• Langley Research Center: Effect of decarburization on notch sensitivity and fatigue-crack-propagation rates in 12 MoV stainless-steel sheet (National Aeronautics and Space Administration, 1961), also by William H. Herrnstein, A. J. McEvily, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of diffusers, shrouds, and mass injection on the starting and operating characteristics of a Mach 5 free jet tunnel (National Aeronautics and Space Administration :, 1971), also by John K. Molloy, J. Wayne Keyes, Ernest A. Mackley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of distributed three-dimensional roughness and surface cooling on boundary-layer transition and lateral spread of turbulence at supersonic speeds (National Aeronautics and Space Administration, 1959), also by Albert L. Braslow, Elmer A. Horton, and Eugene C. Know (page images at HathiTrust)
• Langley Research Center: Effect of eccentricity of the lunar orbit, oblateness of the Earth, and solar gravitational field on lunar trajectories (National Aeronautics and Space Administration, 1960), also by William H. Michael and Robert H. Tolson (page images at HathiTrust)
• Langley Research Center: Effect of electron irradiation on some properties of the Echo II laminate (National Aeronautics and Space Administration :, 1964), also by Thomas G. James (page images at HathiTrust)
• Langley Research Center: Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by William P. Henderson and James R. Burley (page images at HathiTrust)
• Langley Research Center: Effect of engine position and high-lift devices on aerodynamic characteristics of an external-flow jet-flap STOL model (National Aeronautics and Space Administration ;, 1971), also by Charles C. Smith and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of external disturbances and data rate on the response of an automatic landing system capable of curved trajectories (National Aeronautics and Space Administration ;, 1975), also by Windsor L. Sherman (page images at HathiTrust)
• Langley Research Center: Effect of fineness ratio on boattail drag of circular-arc afterbodies having closure ratios of 0.50 with jet exhaust at Mach numbers up to 1.30 (National Aeronautics and Space Administration ;, 1973), also by David E. Reubush and Jack F. Runckel (page images at HathiTrust)
• Langley Research Center: Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 (National Aeronautics and Space Administration, 1959), also by Cornelius Driver (page images at HathiTrust)
• Langley Research Center: Effect of gravitational-model selection on accuracy of lunar orbit determination from short data arcs (National Aeronautics and Space Administration ;, 1969), also by Harold A. Hamer and Katherine G. Johnson (page images at HathiTrust)
• Langley Research Center: Effect of ground proximity on the aerodynamic characteristics of aspect-ratio-1 airfoils with and without end plates (National Aeronautics and Space Administration, 1961), also by Arthur W. Carter and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of ground proximity on the longitudinal aerodynamic characteristics of an aspect-ratio-1 wing with and without wing-tip blowing (National Aeronautics and Space Administration ;, 1974), also by Raymond E. Mineck and Arthur W. Carter (page images at HathiTrust)
• Langley Research Center: Effect of groundboard height on the aerodynamic characteristics of a lifting circular cylinder using tangential blowing from surface slots for lift generation (National Aeronautics and Space Administration, 1961), also by Vernard E. Lockwood and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of image tilt of a virtual image display on simulated transport touchdown performance (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Russell V. Parrish, George G. Steinmetz, William M. Kahlbaum, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by E. Ann Bare, Francis J. Capone, Bobby L. Berrier, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effect of interjet spacing on mixing of multiple coaxial jets in supersonic flow (National Aeronautics and Space Administration ;, 1974), also by A. K. Lorber, Joseph A. Schetz, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Langley Research Center: Effect of interplanetary trajectory options on a manned Mars aerobrake configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Robert D. Braun, Lin C. Hartung, and Richard W. Powell (page images at HathiTrust)
• Langley Research Center: Effect of jet exit vanes on flow pulsations in an open-jet wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by William L. Sellers (page images at HathiTrust)
• Langley Research Center: Effect of leading-edge load constraints on the design and performance of supersonic wings (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Christine M. Darden (page images at HathiTrust)
• Langley Research Center: Effect of LID® processing on the microstructure and mechanical properties of Ti-6Al-4V and Ti-6Al-2Sn-4Zr-2Mo titanium foil-gauge materials (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Linda B. Blackburn (page images at HathiTrust)
• Langley Research Center: Effect of limb darkening on earth radiation incident on a spherical satellite (National Aeronautics and Space Administration ;, 1974), also by S. Katzoff and G. Louis Smith (page images at HathiTrust)
• Langley Research Center: Effect of location of aft-mounted nacelles on longitudinal aerodynamic characteristics of a high-wing transport airplane (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by William Kelly Abeyounis and James C. Patterson (page images at HathiTrust)
• Langley Research Center: Effect of low-speed impact damage and damage location on behavior of composite panels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Dawn C. Jegley (page images at HathiTrust)
• Langley Research Center: Effect of low-velocity impact damage on the compressive strength of graphite-expoxy hat-stiffened panels (National Aeronautics and Space Administration ;, 1977), also by Marvin D. Rhodes, James H. Starnes, Jerry G. Williams, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Christine M. Darden (page images at HathiTrust)
• Langley Research Center: Effect of modifications on aerodynamic characteristics of a single-stage-to-orbit vehicle at Mach 5.9 (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Peter T. Bernot and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effect of motion cues during complex curved approach and landing tasks : a piloted simulation study (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by Charles Scanlon (page images at HathiTrust)
• Langley Research Center: Effect of nacelles on aerodynamic characteristics of an executive-jet model with simulated, partial-chord, laminar-flow-control wing glove (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Richard L. Campbell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer (National Aeronautics and Space Administration, Langley Research Center ;, 1994), also by Meelan Choudhari (page images at HathiTrust)
• Langley Research Center: Effect of outdoor exposure at ambient and elevated temperatures on fatigue life of Ti-6Al-4V titanium alloy sheet in the annealed and the solution-treated and aged condition (National Aeronautics and Space Administration ;, 1974), also by Edward P. Phillips (page images at HathiTrust)
• Langley Research Center: Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Bobby L. Berrier and Francis J. Capone (page images at HathiTrust)
• Langley Research Center: Effect of pressure on structure and NOx formation in CO-Air diffusion flames (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Howard G. Maahs, Irvin M. Miller, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effect of pylon wake with and without pylon blowing on propeller thrust (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Garl L. Gentry, Mohammad Ali Takallu, and Earl R. Booth (page images at HathiTrust)
• Langley Research Center: Effect of ratio of wall boundary-layer thickness to jet diameter on mixing of a normal hydrogen jet in a supersonic stream (National Aeronautics and Space Administration ;, 1974), also by Charles R. McClinton (page images at HathiTrust)
• Langley Research Center: The effect of repeated stressing on the behavior of lithium fluoride crystals (U.S. G.P.O., 1961), also by A. J. McEvily, E. S. Machlin, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The effect of resin composition and fillers on the performance of a molded charring ablator (National Aeronautics and Space Administration, 1963), also by Roger W. Peters and Kenneth L. Wadlin (page images at HathiTrust)
• Langley Research Center: Effect of Reynolds number and engine nacelles on the stalling characteristics of a model of a twin-engine light airplane (National Aeronautics and Space Administration ;, 1972), also by Vernard E. Lockwood (page images at HathiTrust)
• Langley Research Center: Effect of Reynolds number and Mach number on flow angularity probe sensitivity (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Leigh Ann Smith and Jerry B. Adcock (page images at HathiTrust)
• Langley Research Center: Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Robert L. Stallings, Carolyn B. Watson, Milton Lamb, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 ̊clipped-delta-wing orbiter configuration at supersonic mach numbers (U.S. National Aeronautics and Space Administration ;, 1976), also by A. B. Blair and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations (U.S. National Aeronautics and Space Administration ;, 1976), also by David E. Reubush and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of Reynolds number variation on aerodynamics of a hydrogen-fueled transport concept at Mach 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Jim A. Penland and Don C. Marcum (page images at HathiTrust)
• Langley Research Center: The effect of ring distortions on buckling of blunt conical shells (National Aeronautics and Space Administration ;, 1975), also by Walter L. Heard, Wendell B. Stephens, and Melvin S. Anderson (page images at HathiTrust)
• Langley Research Center: Effect of service usage on tensile, fatigue, and fracture properties of 7075-T6 and 7178-T6 aluminum alloys (National Aeronautics and Space Administration ;, 1975), also by Richard A. Everett (page images at HathiTrust)
• Langley Research Center: Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration (National Aeronautics and Space Administrat ion, Scientific and Technical Information Branch ;, 1979), also by Richard J. Re, David E. Reubush, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Bobby L. Berrier, Richard J. Re, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effect of several tail configurations on the stability characteristics of a midwing supersonic-bomber model at mach numbers of 1.60, 1.90, 2.20, and 2.50 (National Aeronautics and Space Administration, 1960), also by R. Franklin Wells and H. Norman Silvers (page images at HathiTrust)
• Langley Research Center: The effect of shearing strain-rate on the ultimate shearing resistance of clay (National Aeronautics and Space Administration, 1976), also by Robert Y. K. Cheng and Old Dominion University (page images at HathiTrust)
• Langley Research Center: Effect of short-term exposure to stereoscopic three-dimensional flight displays on real-world depth perception (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Anthony M. Busquets, Steven P. Williams, Russell V. Parrish, United States. Army Aviation Systems Command, and United States. Army Aviation Research and Development Command (page images at HathiTrust)
• Langley Research Center: Effect of silicon carbide on devitrification of a glass coating for reusable surface insulation (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Philip O. Ransone and United States. National Aeronautics and Space Administration. Scientific and Technical Informaton Office (page images at HathiTrust)
• Langley Research Center: Effect of solidity and inclination on propeller-nacelle force coefficients (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Garl L. Gentry, Mohammad Ali Takallu, and Dana Morris Dunham (page images at HathiTrust)
• Langley Research Center: Effect of specimen thickness on fatigue-crack-growth behavior and fracture toughness of 7075-T6 and 7178-T6 aluminum alloys (National Aeronautics and Space Administration ;, 1973), also by Charles Michael Hudson and J. C. Newman (page images at HathiTrust)
• Langley Research Center: Effect of speed brakes on the supersonic aerodynamic characteristics of a variable-sweep tactical fighter model at Mach numbers from 1.60 to 2.50 (National Aeronautics and Space Administration, 1968), also by Celia S. Richardson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of stress ratio on fatigue-crack growth in 7075-T6 and 2024-T3 aluminum-alloy specimens (National Aeronautics and Space Administration ;, 1969), also by C. M. Hudson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of superconducting solenoid model cores on spanwise iron magnet roll control (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Colin P. Britcher (page images at HathiTrust)
• Langley Research Center: Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Mark C. Frassinelli and George T. Carson (page images at HathiTrust)
• Langley Research Center: Effect of temperature and gap opening rate on the resiliency of candidate solid rocket booster O-ring materials (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Cynthia L. Lach (page images at HathiTrust)
• Langley Research Center: The effect of throat contouring on two-dimensional converging-diverging nozzles at static conditions (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), also by Mary L. Mason, Richard J. Re, Lawrence E. Putnam, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effect of two-dimensional multiple sine-wave protrusions on the pressure and heat-transfer distributions for a flat plate at Mach 6 (National Aeronautics and Space Administration ;, 1968), also by Aubrey M. Cary and E. Leon Morrisette (page images at HathiTrust)
• Langley Research Center: Effect of under-wing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by William Kelly Abeyounis and James C. Patterson (page images at HathiTrust)
• Langley Research Center: Effect of vacuum processing on outgasing within an orbiting molecular shield (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by R. A. Outlaw and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effect of vertical active vibration isolation on tracking performance and ride qualities (National Aeronautics and Space Administration ;, 1972), also by Frank P. DiMasi, Peter C. Calcaterra, Rush E. Allen, and Barry Wright Corporation (page images at HathiTrust)
• Langley Research Center: Effect of vertical-tail location on the aerodynamic characteristics at subsonic speeds of a close-coupled canard configuration (National Aeronautics and Space Administration ;, 1975), also by Jarrett K. Huffman (page images at HathiTrust)
• Langley Research Center: Effect of vertical-tail modifications on the static stability characteristics at mach number of 2.2 of a supersonic vtol airplane model having a broad fuselage and small delta wings (National Aeronautics and Space Administration, 1961), also by Ross B. Robinson and Leroy M. Spearman (page images at HathiTrust; US access only)
• Langley Research Center: Effect of vibration duration on human discomfort (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Sherman A. Clevenson, Jack D. Leatherwood, Thomas K. Dempsey, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: The effect of visual-motion time delays on pilot performance in a simulated pursuit tracking task (National Aeronautics and Space Administration ;, 1977), also by G. Kimball Miller, Donald R. Riley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of weight, density, and heat load on thermal shielding performance of phenolic nylon (National Aeronautics and Space Administration :, 1964), also by Andrew J. Chapman (page images at HathiTrust)
• Langley Research Center: The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model (National Aeronautics and Space Administration ;, 1974), also by Harry H. Heyson (page images at HathiTrust)
• Langley Research Center: Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model (National Aeronautics and Space Administration ;, 1973), also by Charles Christian Smith (page images at HathiTrust)
• Langley Research Center: Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by A. B. Blair and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effect of wing pivot location on longitudinal aerodynamic characteristics of a variable-sweep wing having an M planform (National Aeronautics and Space Administration, 1964), also by William P. Henderson and Edward J. Ray (page images at HathiTrust)
• Langley Research Center: Effect of wing planform and canard location and geometry on the longitudinal aerodynamic characteristics of a close-coupled canard wing model at subsonic speeds (National Aeronautics and Space Administration ;, 1975), also by Blair B. Gloss (page images at HathiTrust)
• Langley Research Center: Effect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration (National Aeronautics and Space Administration ;, 1972), also by Louis E. Clark and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effect of winglets on a first-generation jet transport wing : III, pressure and spanwise load distributions for a semispan model at Mach 0.30 (National Aeronautics and Space Administration ;, 1977), also by Lawrence C. Montoya, Peter F. Jacobs, Stuart G. Flechner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The effect of winglets on the static aerodynamic stability characteristics of a representative second generation jet transport model (U.S. National Aeronautics and Space Administration ;, 1976), also by Peter F. Jacobs, Stuart G. Flechner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The effectiveness of an oculometer training tape on pilot and copilot trainees in a commercial flight training program (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Dennis H. Jones, Raymond H. Kirby, Glynn D. Coates, Old Dominion University. Research Foundation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: The effectiveness of incorporating a real-time oculometer system in a commercial flight training program (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Dennis H. Jones, Raymond H. Kirby, Glynn D. Coates, Old Dominion University. Research Foundation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of 1- and 2-MeV electrons on photomultiplier tubes (National Aeronautics and Space Administration ;, 1976), also by Marvin E. Beatty, Barry D. Meredith, and William J. Debnam (page images at HathiTrust)
• Langley Research Center: Effects of 1 MeV electrons on ceria-doped solar cell cover glass (National Aeronautics and Space Administration ;, 1973), also by Gilbert A. Haynes (page images at HathiTrust)
• Langley Research Center: Effects of 1.2 and 0.30 Mev electrons on the optical transmission properties of several transparent materials (National Aeronautics and Space Administration :, 1965), also by Gilbert A. Haynes and William E. Miller (page images at HathiTrust)
• Langley Research Center: Effects of 3 spanwise twist variations on the longitudinal aerodynamic characteristics of a thin 45 degree sweptback highly tapered wing at transonic speeds (National Aeronautics and Space Administration, 1959), also by John P. Mugler (page images at HathiTrust)
• Langley Research Center: Effects of a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 (National Aeronautics and Space Administration, 1960), also by Emma Jean Landrum (page images at HathiTrust)
• Langley Research Center: Effects of a modified leading edge on noise and boundary-layer transition in a rod-wall sound shield at mach 5 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Theodore R. Creel, W. E. Zorumski, Ivan E. Beckwith, Barbara B. Holley, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of activity interference on annoyance due to aircraft noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Kelli F. Willshire, Clemans A. Powell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Linda S. Bangert, David E. Reubush, and Laurence D. Leavitt (page images at HathiTrust)
• Langley Research Center: Effects of aircraft noises on the sleep of women (National Aeronautics and Space Administration ;, 1972), also by Jerome S. Lukas, Mary E. Dobbs, and Stanford Research Institute (page images at HathiTrust)
• Langley Research Center: Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by John T. Batina (page images at HathiTrust)
• Langley Research Center: The effects of an autopilot on airplane responses to turbulence with emphasis on tail loads (National Aeronautics and Space Administration ;, 1973), also by Boyd Perry and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of axisymmetric and normal air jet plumes and solid plume on cylindrical afterbody pressure distributions at Mach numbers from 1.65 to 2.50 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Peter F. Covell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of background noise on total noise annoyance (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Kelli F. Willshire and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of body and fin deflections on the aerodynamic characteristics in pitch of a 0.065-scale model of a four-stage rocket configuration at Mach numbers of 1.41 and 1.82 (National Aeronautics and Space Administration, 1959), also by Ross B. Robinson (page images at HathiTrust)
• Langley Research Center: Effects of bottom-structure flexibility of water landing loads of Apollo spacecraft models (National Aeronautics and Space Administration ;, 1969), also by Sandy M. Stubbs and Melvin E. Hathaway (page images at HathiTrust)
• Langley Research Center: Effects of cable geometry and aircraft attitude on the accuracy of a magnetic leader cable system for aircraft guidance during rollout and turnoff (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by W. Thomas Bundick and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of camber and twist on the aerodynamic characteristics of parawings having nominal aspect ratios of 3 and 65 (NASA, 1963), also by Edward C. Polhamus, Rodger L. Naeseth, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of canard planform and wing-leading-edge modification on low-speed longitudinal aerodynamic characteristics of a canard airplane configuration (National Aeronautics and Space Administration, 1961), also by Bernard Spencer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of canted forward faces on the static longitudinal stability characteristics of the escape and exit configurations of a project mercury capsule model at a mach number of 2.01 (National Aeronautics and Space Administration, 1960), also by Roy V. Harris, Ross B. Robinson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aeroacoustic codes (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by K. K. Ahuja, J. Mendoza, and Georgia Institute of Technology (page images at HathiTrust)
• Langley Research Center: Effects of certain control-system nonlinearities on stability and pointing of an attached double-gimbal experiment package in presence of random crew-motion disturbances (National Aeronautics and Space Administration ;, 1973), also by J. D. Shaughnessy, Vilas D. Nene, and Nelson J. Groom (page images at HathiTrust)
• Langley Research Center: Effects of changing stress amplitude on the rate of fatigue-crack propagation in two aluminum alloys (National Aeronautics and Space Administration, 1961), also by C. M. Hudson, Herbert F. Hardrath, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of cloud cover on selection of recovery sites for future earth orbital missions (National Aeronautics and Space Administration, 1969), also by Paul F. Holloway and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of combining vertical and horizontal information into a primary flight display (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by Terence S. Abbott, Mark Nataupsky, and George G. Steinmetz (page images at HathiTrust)
• Langley Research Center: Effects of control-response characteristics on the capability of a helicopter for use as a gun platform (National Aeronautics and Space Administration :, 1960), also by Robert J. Pegg and Andrew B. Connor (page images at HathiTrust)
• Langley Research Center: Effects of conventional and square stores on the longitudinal aerodynamic characteristics of a fighter aircraft model at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by William J. Monta and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Effects of corner radius on stagnation-point velocity gradients on blunt axisymmetric bodies (National Aeronautics and Space Administration, 1965), also by Ernest V. Zoby, Edward M. Sullivan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of curved approach paths and advanced displays on pilot scan patterns (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Randall L. Harris, Randolph W. Mixon, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of dielectric covers over cross slots in a rectangular waveguide (National Aeronautics and Space Administration ;, 1967), also by Marion Crawford Bailey (page images at HathiTrust)
• Langley Research Center: Effects of dielectric covers over shunt slots in a waveguide (National Aeronautics and Space Administration :, 1964), also by W. F. Croswell and Robert B. Higgins (page images at HathiTrust)
• Langley Research Center: Effects of digital altimetry on pilot workload (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Randall L. Harris and Bobby J. Glover (page images at HathiTrust)
• Langley Research Center: Effects of eccentricities and lateral pressure on the design of stiffened compression panels (National Aeronautics and Space Administration ;, 1972), also by Gary L. Giles, Melvin S. Anderson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The effects of environmental exposure on reusable surface insulation for space shuttle (National Aeronautics and Space Administration ;, 1975), also by Philip O. Ransone and J. D. Morrison (page images at HathiTrust)
• Langley Research Center: Effects of errors on decoupled control systems (National Aeronautics and Space Administration, Scientific and Technical Information Service ;, 1978), also by Harold A. Hamer, Katherine G. Johnson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Effects of fiber, matrix, and interphase on carbon fiber composite compression strength (National Aeronautics and Space Administration, Langley Research Center, 1994), also by John A. Nairn, Willard D. Bascom, and Sheila I. Harper (page images at HathiTrust)
• Langley Research Center: Effects of fiber/matrix interactions on the properties of graphite/epoxy composites (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Paul E. McMahon, Lincoln Ying, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Celanese Corporation (page images at HathiTrust)
• Langley Research Center: Effects of fineness and closure ratios on boattail drag of circular-arc afterbody models with jet exhaust at Mach numbers up to 1.3 (National Aeronautics and Space Administration ;, 1973), also by David E. Reubush (page images at HathiTrust)
• Langley Research Center: Effects of forebody geometry on subsonic boundary-layer stability (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by S. S. Dodbele, Vigyan Research Associates, and Québec) International Conference on Numerical Methods in Laminar and Turbulent Flow (5th : 1987 : Montréal (page images at HathiTrust)
• Langley Research Center: Effects of fragmentation parameter variations on estimates of galactic cosmic ray exposure : dose sensitivity studies for aluminum shields (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Lawrence W. Townsend (page images at HathiTrust)
• Langley Research Center: Effects of fuselage forebody geometry on low-speed lateral-directional characteristics of twin-tail fighter model at high angles of attack (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Peter C. Carr, William P. Gilbert, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Hugh L. Dryden Flight Research Center (page images at HathiTrust)
• Langley Research Center: Effects of geometric variables on the performance of a probe for direct measurement of free-stream stagnation pressure in supersonic flow (National Aeronautics and Space Administration ;, 1975), also by Lana M. Couch (page images at HathiTrust)
• Langley Research Center: Effects of geometry and jet velocity on noise associated with an upper-surface-blowing model (National Aeronautics and Space Administration ;, 1977), also by Lorenzo R. Clark, James C. Yu, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of grazing flow on the steady-state flow resistance and acoustic impedance of thin porous-faced liners : A.S. Hersh and B. Walker. (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by A. S. Hersh, Bruce Walker, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Effects of gyroscopic cross coupling between pitch and yaw on the handling qualities of VTOL aircraft (National Aeronautical and Space Administration, 1961), also by John F. Garren and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of inlet-guide-vane configuration and relative blade velocity on noise from axial-flow compressors (National Aeronautics and Space Administration ;, 1970), also by David Chestnutt and Lorenzo R. Clark (page images at HathiTrust)
• Langley Research Center: Effects of installation of F101 DFE exhaust nozzles on the afterbody-nozzle characteristics of the F-14 airplane (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by David E. Reubush, John R. Carlson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of jet exhaust gas properties on exhaust simulation and afterbody drag (National Aeronautics and Space Administration ;, 1975), also by William B. Compton (page images at HathiTrust)
• Langley Research Center: Effects of jet-exhaust location on the longitudinal aerodynamic characteristics of a jet V/STOL model (National Aeronautics and Space Administration ;, 1969), also by Arthur W. Carter and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of leading-edge bluntness and ramp deflection angle on laminar boundary-layer separation in hypersonic flow (National Aeronautics and Space Administration ;, 1966), also by James C. Townsend (page images at HathiTrust)
• Langley Research Center: Effects of leading-edge camber on low-speed characteristics of slender delta wings (National Aeronautics and Space Administration ;, 1972), also by W. H. Wentz and Wichita State University (page images at HathiTrust)
• Langley Research Center: Effects of leading-edge sweep angle and design lift coefficient on performance of a modified arrow wing at a design Mach number of 2.6 (National Aeronautics and Space Administration ;, 1974), also by Robert J. Mack (page images at HathiTrust)
• Langley Research Center: Effects of loading sequence for notched specimens under high-low two-step fatigue loading (National Aeronautics and Space Administration ;, 1971), also by John H. Crews and United States. National Aeronautical and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of longtime environmental exposure on mechanical properties of sheet materials for a supersonic transport (National Aeronautics and Space Administration ;, 1968), also by Richard A. Pride (page images at HathiTrust)
• Langley Research Center: Effects of Mach number on pitot-probe displacment in a turbulent boundary layer (National Aeronautics and Space Administration ;, 1974), also by Jerry M. Allen (page images at HathiTrust)
• Langley Research Center: Effects of magnetically induced eddy-current torques on spin motions of an earth satellite (National Aeronautics and Space Administration :, 1965), also by G. Louis Smith (page images at HathiTrust)
• Langley Research Center: Effects of material composition on the ablation performance of low-density elastomeric ablators (National Aeronautics and Space Administration ;, 1973), also by Stephen S. Tompkins and Walter P. Kabana (page images at HathiTrust)
• Langley Research Center: Effects of model error on control of large flexible space antenna with comparisons of decoupled and linear quadratic regulator control procedures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Harold A. Hamer and Katherine G. Johnson (page images at HathiTrust)
• Langley Research Center: Effects of modifications to the space shuttle entry guidance and control systems (National Aeronautics and Space Administration ;, 1976), also by Richard W. Powell, Lawrence F. Rowell, Howard W. Stone, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of nacelle configuration/position on performance of subsonic transport (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by L. H. Bangert, D. K. Krivec, R. N. Segall, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lockheed-California Company (page images at HathiTrust)
• Langley Research Center: Effects of noise on the performance of a memory-decision-response task (National Aeronautics and Space Administration ;, 1972), also by Ben William Lawton and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The effects of nonuniform swash-plate stiffness on coupled blade-control system dynamics and stability : Part 1. Analysis and application (National Aeronautics and Space Administration, 1971), also by Vincent James Piarulli, United States National Aeronautics and Space Administration, and Rochester Applied Sciences Associates (page images at HathiTrust)
• Langley Research Center: The effects of nonuniform swash-plate stiffness on coupled blade-control system dynamics and stability. Part II, Computer program listing (National Aeronautics and Space Administration ;, 1971), also by Vincent J. Piarulli and inc Rochester Applied Science Associates (page images at HathiTrust)
• Langley Research Center: Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2 (U.S. National Aeronautics and Space Administration ;, 1976), also by Francis J. Capone (page images at HathiTrust)
• Langley Research Center: Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model (National Aeronautics and Space Administration ;, 1975), also by David E. Reubush and Charles E. Mercer (page images at HathiTrust)
• Langley Research Center: Effects of orientation of the acceleration vector on burning-rate augmentation (National Aeronautics and Space Administration ;, 1972), also by G. Burton Northam (page images at HathiTrust)
• Langley Research Center: Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor (National Aeronautics and Space Administration, 1986), also by Arthur E. Phelps, Susan L. Althoff, United States. Army Aviation Research and Technology Activity. Aerostructures Directorate, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and United States. Army Aviation Systems Command (page images at HathiTrust)
• Langley Research Center: Effects of precursor heating on radiative and chemially reacting viscous flow around a Jovian entry body (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by S. N. Tiwari, Kuo-Yen Szema, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of propeller rotation direction on airplane interior noise levels (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Conrad M. Willis, Edward F. Daniels, and William H. Mayes (page images at HathiTrust)
• Langley Research Center: Effects of repetition rate and impulsiveness of simulated helicopter rotor noise on annoyance (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Clemans A. Powell, David A. McCurdy, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of Reynolds number and model support on the supersonic aerodynamic chacteristics of a 140° included-angle cone (National Aeronautics and Space Administration ;, 1974), also by Charles D. Trescot, Dorothy T. Howell, and Clarence A. Brown (page images at HathiTrust)
• Langley Research Center: Effects of road-traffic background noise on judgments of individual airplane noises (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Clemans A. Powell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of service environments on aluminum-brazed titanium (ABTi) (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by W. L. Cotton, Boeing Commercial Airplane Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Effects of shunt capacitance on transient effects caused by electron irradiation of a polyethylene terephthalate insulated ribbon wire (National Aeronautics and Space Administration ;, 1966), also by William E. Miller and Donald H. Phillips (page images at HathiTrust)
• Langley Research Center: Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Jeffery A. Yetter, Laurence D. Leavitt, Joint Institute for Advancement of Flight Sciences, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of simulated space environment on Skylab parasol material (National Aeronautics and Space Administration ;, 1974), also by Wayne S. Slemp (page images at HathiTrust)
• Langley Research Center: Effects of sound level fluctuations on annoyance caused by aircraft-flyoter noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by David A. McCurdy and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of space exposure on metals flown on the Long Duration Exposure Facility (National Aeronautics and Space Administration, Langley Research Center, 1995), also by H. Gary Pippin and R. J. Bourassa (page images at HathiTrust)
• Langley Research Center: Effects of spanwise blowing on the pressure field and vortex-lift characteristics of a 44 ̊swept trapezoidal wing (National Aeronautics and Space Administration ;, 1975), also by James F. Campbell (page images at HathiTrust)
• Langley Research Center: Effects of specimen preparation on the accuracy of electromagnetic property measurements of solid materials with an automatic network analyzer (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Edward R. Long (page images at HathiTrust)
• Langley Research Center: Effects of stiffener/rib separation on damage growth and residual strength (Federal Aviation Administration, Office of Aviation Research ;, 1996), also by H. P. Kan, M. Mahler, Northrop Corporation. Military Aircraft Division, and United States. Office of Aviation Research (page images at HathiTrust)
• Langley Research Center: Effects of structural damping on flutter of stressed panels (National Aeronautics and Space Administration ;, 1969), also by Charles P. Shore and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of temperature on noise of bypass jets as measured in the Langley noise research facility (National Aeronautics and Space Administration, 1964), also by George T. Kantarges, Jimmy M. Cawthorn, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of the atmospheric-lithostatic pressure ratio on explosive craters in dry soil (National Aeronautics and Space Administration, 1971), also by Robert W. Herr and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by David E. Reubush and Bobby L. Berrier (page images at HathiTrust)
• Langley Research Center: Effects of thermal cycling on graphite-fiber-reinforced 6061 aluminum (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Gregory A. Dries and Stephen S. Tompkins (page images at HathiTrust)
• Langley Research Center: Effects of three transmission models in the rotational water-vapor band on radiance calculations and constituent inferences (National Aeronautics and Space Administration, 1971), also by Ruth I. Whitman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Lawrence E. Putnam (page images at HathiTrust)
• Langley Research Center: Effects of variable turbine area on subsonic cruise performance of turbojets designed for supersonic application (National Aeronautics and Space Administration :, 1970), also by Arvid L. Keith and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of various assumptions on the calculated liquid fraction in isentropic saturated equilibrium expansions (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), also by Joseph W. Bursik, Robert M. Hall, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: The effects of various combinations of damping and control power on helicopter handling qualities during both instrument and visual flight (National Aeronautics and Space Administration, 1959), also by Seymour Salmirs and Robert J. Tapscott (page images at HathiTrust)
• Langley Research Center: Effects of various experimental parameters on errors in triangulation solution of elongated object in space (National Aeronautics and Space Administration ;, 1975), also by Sheila Ann T. Long (page images at HathiTrust)
• Langley Research Center: Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds (National Aeronautics and Space Administration, 1960), also by Walter B. Olstad (page images at HathiTrust)
• Langley Research Center: Effects of vibrational nonequilibrium on the inviscid design of an axisymmetric nozzle for hypersonic flow (National Aeronautics and Space Administration ;, 1975), also by John Benjamin Anders (page images at HathiTrust)
• Langley Research Center: Effects of vortex flaps on the low-speed aerodynamic characteristics of an arrow wing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Long P. Yip, Daniel G. Murri, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Effects of wing height on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a 70 degree delta wing (National Aeronautics and Space Administration, 1960), also by Cornelius Driver and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by William P. Henderson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Effects of wing-leading-edge modifications on a full-scale, low-wing general aviation airplane : wind-tunnel investigation of high-angle-of-attack aerodynamic characteristics (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by William A. Newsom, Dale R. Satran, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Joseph L. Johnson (page images at HathiTrust)
• Langley Research Center: Effects of wing leading-edge radius and Reynolds number on longitudinal aerodynamic characteristics of highly swept wing-body configurations at subsonic speeds (National Aeronautics and Space Administration ;, 1976), also by William P. Henderson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers 3.96 and 4.63 (National Aeronautics and Space Administration ;, 1966), also by Maurice O. Feryn (page images at HathiTrust)
• Langley Research Center: Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers 1.57, 2.16, and 2.87 (National Aeronautics and Space Administration :, 1965), also by Royce L. McKinney, Lloyd S. Jernell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Charles L. Ruhlin, K. S. Nagaraja, and Kumar G. Bhatia (page images at HathiTrust)
• Langley Research Center: Effects of winglets on first-generation jet transport wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Stuart G. Flechner and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: The effects of winglets on low aspect ratio wings at supersonic Mach numbers (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by James A. Keenan, John Kuhlman, and West Virginia University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• Langley Research Center: The effects on propulsion-induced aerodynamic forces of vectoring a partial-span rectangular jet at Mach numbers from 0.40 to 1.20 (National Aeronautics and Space Administration ;, 1975), also by Francis J. Capone (page images at HathiTrust)
• Langley Research Center: An efficient HZETRN : (a galactic cosmic ray transport code) (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Judy L. Shinn and John W. Wilson (page images at HathiTrust)
• Langley Research Center: Efficient multitasking of Choleski matrix factoriztion on CRAY supercomputers (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Andrea L. Overman and Eugene L. Poole (page images at HathiTrust)
• Langley Research Center: Efficient solutions to the Euler equations for supersonic flow with embedded subsonic regions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Robert W. Walters and Douglas L. Dwoyer (page images at HathiTrust)
• Langley Research Center: Effluent monitoring of the December 10, 1974, Titian III-E launch at Air Force Eastern Test Range, Florida (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Dewey E. Wornom, David C. Woods, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Effluent sampling of Scout "D" and Delta launch vehicle exhausts (National Aeronautics and Space Administration ;, 1974), also by William C. Hulten (page images at HathiTrust)
• Langley Research Center: Eigensystem realization algorithm modal identification experiences with Mini-Mast (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Richard S. Pappa, Christopher Noll, and Axel Schenk (page images at HathiTrust)
• Langley Research Center: Eigenvalue extraction in NASTRAN by the Tridiagonal Reduction (FEER) Method : real eigenvalue analysis (National Aeronautics and Space Administration ;, 1976), also by Malcolm Newman, Paul F. Flanagan, and Analytical Mechanics Associates (page images at HathiTrust)
• Langley Research Center: Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads (National Aeronautics and Space Administration ;, 1973), also by A. V. Viswanathan, M. Tamekuni, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Elastic deformation effects on aerodynamic characteristics for a high-aspect-ratio supercritical-wing model (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), also by Judith J. Watson (page images at HathiTrust)
• Langley Research Center: Elastic stability of laminated, flat and curved, long rectangular plates subjected to combined inplane loads (National Aeronautics and Space Administration ;, 1974), also by A. V. Viswanathan, L. L. Baker, M. Tamekuni, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: An elastoplastic analysis of a uniaxially loaded sheet with an interference-fit bolt (National Aeronautics and Space Administration ;, 1974), also by John H. Crews (page images at HathiTrust)
• Langley Research Center: Electrical characteristics of Pyrrone polymers (National Aeronautics and Space Administration ;, 1969), also by P. J. Reucroft and Pa.). Research Laboratories Franklin Institute (Philadelphia (page images at HathiTrust)
• Langley Research Center: Electroencephalographic monitoring of complex mental tasks (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Raul Guisado and Center for Neurodiagnostic Study (page images at HathiTrust)
• Langley Research Center: Electromagnetic and scalar diffraction by a right-angled wedge with a uniform surface impedance (National Aeronautics and Space Administration ;, 1974), also by Y. M. Hwang and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: The electromagnetic radiation environment of a satellite. (National Aeronautics and Space Administration, 1962), also by S. Katzoff and Jerry L. Modisette (page images at HathiTrust)
• Langley Research Center: The electromagnetic radiation from simple sources in the presence of a homogeneous dielectric sphere (National Aeronautics and Space Administration ;, 1973), also by V. Bradford Mason and University of Michigan. Radiation Laboratory (page images at HathiTrust)
• Langley Research Center: Electromagnetism in moving, conducting media (National Aeronautics and Space Administration] ;, 1968), also by Rudolph M. Kalafus, University of Michigan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Electron and proton absorption calculations for a graphite/epoxy composite model (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Edward R. Long and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Electron-induced luminescence in optical materials (National Aeronautics and Space Administration, 1971), also by John Romanko, P. R. Cheever, J. K. Miles, United States National Aeronautics and Space Administration, and General Dynamics. Convair Aerospace Division (page images at HathiTrust)
• Langley Research Center: Electron spectroscopy for chemical analysis (ESCA) study of atmospheric particles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by John G. Dillard, James P. Wightman, Roland D. Seals, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Electron stimulated desorption of atomic oxygen from silver (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by R. A. Outlaw (page images at HathiTrust)
• Langley Research Center: An Electronic control for an electrohydraulic active control aircraft landind gear (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Irving Ross, Ralph Edson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: An electronic system for measuring thermophysical properties of wind tunnel models (National Aeronautics and Space Administration ;, 1975), also by Richard R. Corwin, Joseph S. Kramer, and Beta Industries (page images at HathiTrust)
• Langley Research Center: Electronics reliability and measurement technology : proceedings of a conference (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987), also by Joseph S. Heyman (page images at HathiTrust)
• Langley Research Center: Elemental characteristics of aerosols emitted from a coal-fired heating plant (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Jag J. Singh, G. S. Khandelwal, Old Dominion University, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Elevated-temperature application of the IITRI compression test fixture for graphite/polyimide filmentary composites (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by B. Basava Raju, Paul A. Cooper, Charles J. Camarda, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: The elevation, slope, and curvature spectra of a wind roughened sea surface (National Aeronautics and Space Administration, 1973), also by Willard J. Pierson, Robert A. Stacy, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Emergency in-flight egress opening for general aviation aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Laurence J. Bement and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Emittance, catalysis, and dynamic oxidation of Ti-14Al-21Nb (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by K. E. Wiedemann, Sankara Narayan Sankaran, and R. K. Clark (page images at HathiTrust)
• Langley Research Center: Emotionality in response to aircraft noise : a report of developmental work (National Aeronautics and Space Administration ;, 1975), also by Patsy A. Klaus and Institute for Applied Technology (U.S.). Technical Analysis Division (page images at HathiTrust)
• Langley Research Center: An empirical method for determining static distributed aerodynamic loads on axisymmetric multistage launch vehicles (National Aeronautics and Space Administration ;, 1966), also by Ralph J. Muraca (page images at HathiTrust)
• Langley Research Center: Empirical source noise prediction method with application to subsonic coaxial jet mixing noise (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by W. E. Zorumski, Donald S. Weir, Kentron International, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Empirically determined wind and scale effects on hot gas recirculation characteristics of jet V/Stol aircraft (National Aeronautics and Space Administration, 1969), also by Patrick E. Ryan, Wayne J. Cosgrove, and Bell Aerospace Corporation. Bell Aerosystems Company (page images at HathiTrust; US access only)
• Langley Research Center: Energy transfer rates of an integrated life support system during manned and intermittently manned tests (National Aeronautics and Space Administration ;, 1971), also by O. Karl Houck and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Engine isolation for structural-borne interior noise reduction in a general aviation aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981), also by James F. Unruh and Dennis C. Scheidt (page images at HathiTrust)
• Langley Research Center: Engine monitoring display study (National Aeronautics and Space Administration, 1992), also by Mary E. Hornsby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Engineering and scientific data management : proceedings of a conference sponsored by the Langley Research Center, the Institute for Computer Applications in Science and Engineering (ICASE), and the George Washington University Joint Institute for Advancement of Flight Sciences, Hampton, Virginia, and held at Langley Research Center, May 18-19, 1978. (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Joint Institute for Advancement of Flight Sciences, Institute for Computer Applications in Science and Engineering, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Engineering prediction of turbulent skin friction and heat transfer in high-speed flow (National Aeronautics and Space Administration ;, 1974), also by Aubrey M. Cary and Mitchel H. Bertram (page images at HathiTrust)
• Langley Research Center: An engineering procedure for calculating compressive strength of isogrid cylindrical shells with buckled skin (National Aeronautics and Space Administration ;, 1976), also by Walter L. Heard, Paul Slysh, Melvin S. Anderson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An enhanced integrated aerodynamic load/dynamic optimization procedure for helicopter rotor blades (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Aditi Chattopadhyay, Y. Danny Chiu, Lockheed Engineering & Sciences Company, and Inc Analytical Services & Materials (page images at HathiTrust)
• Langley Research Center: Entry dynamics of space shuttle orbiter with longitudinal stability and control uncertainties at supersonic and hypersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Howard W. Stone, Richard W. Powell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Entry thermal protection. (National Aeronautics and Space Administration, 1968), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Environmental effects on space shuttle reusable surface insulation coated with reaction cured glass (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Philip O. Ransone, John E. Minster, J. D. Morrison, John F. Kennedy Space Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Environmental exposure effects on composite materials for commercial aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Martin N. Gibbins, Daniel J. Hoffman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Environmental protection requirements for scout/shuttle auxiliary stages (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by G. L. Qualls and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An equation for vortex motion including effects of buoyancy and sources with applications to tornadoes. (National Aeronautics and Space Administration :, 1970), also by Robert C. Costen and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Equilibrium chemical reaction of supersonic hydrogen-air jets : the Alma computer program (National Aeronautics and Space Administration ;, 1977), also by S. Elghobashi, D. B. Spalding, Fluid Mechanics and Thermal Systems, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Equipment and procedures for glass-bead peening titanium-alloy tanks (National Aeronautics and Space Administration ;, 1968), also by Thomas T. Bales, W. Barry Lisagor, and Charles R. Manning (page images at HathiTrust)
• Langley Research Center: The equipotential space-suit design concept and its application to a space-suit elbow joint (National Aeronautics and Space Administration ;, 1969), also by Donald E. Barthlome and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Error analysis of Householder transformations as applied to the standard and generalized Eigenvalue problems (National Aeronautics and Space Administration ;, 1974), also by Robert C. Ward (page images at HathiTrust)
• Langley Research Center: Error analysis of input-noise-temperature measurements of low-noise amplifiers (National Aeronautics and Space Administration ;, 1969), also by Hans-Juergen C. Blume and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Error analysis of several methods of determining vehicle position in earth-moon space from simultaneous onboard optical measurements (National Aeronautics and Space Administration, 1963), also by Harold A. Hamer, Alton P. Mayo, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: Estimates of attenuation and reflection of telemetering signals by ionized flow fields surrounding typical reentry bodies (National Aeronautics and Space Administration, 1963), also by Anthony J. Russo and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: Estimates of galactic cosmic ray shielding requirements during solar minimum (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Lawrence W. Townsend (page images at HathiTrust)
• Langley Research Center: Estimates of minimum energy requirements for range-controlled return of a nonlifting satellite from a circular orbit (National Aeronautics and Space Administration, 1961), also by Charles M. Jackson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Estimation of airplane stability and control derivatives from large amplitude longitudinal maneuvers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by James G. Batterson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Estimation of attainable leading-edge thrust for wings at subsonicaand supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Harry W. Carlson, Raymond L. Barger, Robert J. Mack, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Estimation of fan pressure ratio requirements and operating performance for the national transonic facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Blair B. Gloss, Donna Nystrom, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Estimation of leading-edge thrust for supersonic wings of arbitrary planform (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Harry W. Carlson, Robert J. Mack, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Estimation of variance by a recursive equation (National Aeronautics and Space Administration, 1969), also by M. Melvin Bruce and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Harry W. Carlson, Robert J. Mack, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Euler technology assessment for preliminary aircraft design employing OVERFLOW code with multiblock structured-grid method (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by David A. Treiber and Dennis A. Muilenburg (page images at HathiTrust)
• Langley Research Center: Euler technology assessment program for preliminary aircraft design employing SPLITFLOW code with cartesian unstructured grid method (National Aeronautics and Space Administration, Langley Research Center, 1995), also by Dennis B. Finley (page images at HathiTrust)
• Langley Research Center: EVA assembly of a large space structure element (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Laurence J. Bement, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Langley Research Center: Evaluation of a computer-generated perspective tunnel display for flight-path following (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Arthur J. Grunwald, Jack J. Hatfield, James B. Robertson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An evaluation of a constrained test method for obtaining free body responses (National Aeronautics and Space Administration ;, 1973), also by A. Berman, F. D. Bartlett, N. Giansante, and Kaman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Evaluation of a flash X-ray technique for recession measurements in ablative materials (National Aeronautics and Space Administration ;, 1970), also by William D. Brewer, Philip C. Kassel, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Evaluation of a gravity-simulation technique for studies of man's self-locomotion in lunar environment (National Aeronautics and Space Administration :, 1964), also by Donald E. Hewes and Amos A. Spady (page images at HathiTrust)
• Langley Research Center: Evaluation of a hybrid anisotropic, multilayered, quadrilateral finite element (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by James Campbell Robinson, Charles L. Blackburn, University of Tennessee at Nashville, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Evaluation of a metal shear web selectively reinforced with filamentary composites for space shuttle application (National Aeronautics and Space Administration ;, 1974), also by J. H. Laakso, J. W. Straayer, and Boeing Aerospace Company (page images at HathiTrust)
• Langley Research Center: Evaluation of a scale-model experiment to investigate long-range acoustic propagation (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by Tony L. Parrott, Ingrid A. Carlberg, and Gerry L. McAninch (page images at HathiTrust)
• Langley Research Center: Evaluation of a technique for measuring ion energy loss in vapor-deposited materials (National Aeronautics and Space Administration ;, 1969), also by Joseph S. Heyman (page images at HathiTrust)
• Langley Research Center: Evaluation of a vortex model of turbulent cavity flow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Jay C. Hardin, P. J. W. Block, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Evaluation of active cooling systems for a Mach 6 hypersonic transport airframe (National Aeronautics and Space Administration ;, 1971), also by R. G. Helenbrook, F. M. Anthony, W. A. Mcconarty, and Bell Aerospace Company (page images at HathiTrust)
• Langley Research Center: Evaluation of adhesive materials used on the long duration exposure facility (National Aeronautics and Space Administration, Langley Research Center, 1995), also by H. W. Dursch, H. Gary Pippin, and B. K. Keough (page images at HathiTrust)
• Langley Research Center: Evaluation of braking performance of a light, twin-engine airplane on grooved and ungrooved pavements (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), also by Thomas J. Yager, Perry L. Deal, W. Pelham Phillips, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Evaluation of bulk calorimeter and heat balance for determination of supersonic combustor efficiency (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by C. R. McClinton, G. Y. Anderson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Evaluation of compressible-flow Preston tube calibrations (National Aeronautics and Space Administration ;, 1973), also by Jerry M. Allen (page images at HathiTrust)
• Langley Research Center: Evaluation of configuration changes on optimum structural designs for a Mars entry capsule (National Aeronautics and Space Administration ;, 1969), also by Gerald A. Cohen and Philco-Ford Corporation (page images at HathiTrust)
• Langley Research Center: Evaluation of control laws and actuator locations for control systems applicable to deformable astronomical telescope mirrors (National Aeronautics and Space Administration ;, 1973), also by Aaron J. Ostroff (page images at HathiTrust)
• Langley Research Center: Evaluation of effectiveness of various devices for attenuation of trailing vortices based on model tests in a large towing basin (National Aeronautics and Space Administration ;, 1973), also by Karl L. Kirkman, Alex Goodman, Clinton E. Brown, and inc Hydronautics (page images at HathiTrust)
• Langley Research Center: An evaluation of effects of flexibility on wing strains in rough air for a large swept-wing airplane by means of experimentally determined frequency-response functions with an assessment of random-process techniques employed (U.S. G.P.O., 1960), also by Thomas L. Coleman, May T. Meadows, Harry Press, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Evaluation of electrolytic tilt sensors for measuring model angle of attack in wind tunnel tests (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Douglas T. Wong (page images at HathiTrust)
• Langley Research Center: Evaluation of emergency-locator-transmitter performance in real and simulated crash tests (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Huey D. Carden and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Evaluation of energy absorption of new concepts of aircraft composite subfloor intersections (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Lisa E. Jones and Huey D. Carden (page images at HathiTrust)
• Langley Research Center: Evaluation of fault-tolerant parallel-processor architectures over long space missions (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Sally C. Johnson (page images at HathiTrust)
• Langley Research Center: An Evaluation of flight path formats head-up and head-down (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by George A. Sexton (page images at HathiTrust)
• Langley Research Center: Evaluation of flow properties behind 120-̊ and 140-̊included-angle cones and a Viking '75 entry vehicle at Mach numbers from 1.60 to 3.95 (National Aeronautics and Space Administration ;, 1973), also by Clarence A. Brown and James F. Campbell (page images at HathiTrust)
• Langley Research Center: Evaluation of flow quality in two large NASA wind tunnels at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Bill Harvey, F. Kevin Owen, P. Calvin Stainback, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An evaluation of gemini hand controllers and instruments for docking (National Aeronautics and Space Administration ;, 1965), also by Byron M. Jacquet and Donald R. Riley (page images at HathiTrust)
• Langley Research Center: Evaluation of GPS position and attitude determination for automated rendezvous and docking missions (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Marc David DiPrinzio and Robert H. Tolson (page images at HathiTrust)
• Langley Research Center: Evaluation of helicopter noise due to blade-vortex interaction for five tip configurations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Danny R. Hoad, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Evaluation of installed performance of a wing-tip-mounted pusher turboprop on a semispan wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by James C. Patterson and Glynn R. Bartlett (page images at HathiTrust)
• Langley Research Center: An evaluation of linearized vortex theory as applied to single and multiple rotors hovering in and out of ground effect (National Aeronautics and Space Administration, 1959), also by Harry H. Heyson (page images at HathiTrust)
• Langley Research Center: Evaluation of magnesium-aluminum eutectic to improve combustion efficiency in low burning-rate propellants (National Aeronautics and Space Administration ;, 1973), also by G. Burton Northam and Edward M. Sullivan (page images at HathiTrust)
• Langley Research Center: Evaluation of seals and lubricants used on the long duration exposure facility (National Aeronautics and Space Administration, Langley Research Center, 1994), also by H. W. Dursch, H. Gary Pippin, and B. K. Keough (page images at HathiTrust)
• Langley Research Center: An evaluation of string theory for the prediction of dynamic tire properties using scale model aircraft tires (National Aeronautics and Space Administration ;, 1972), also by Samuel K. Clark, G. H. Nybakken, Richard N. Dodge, and University of Michigan (page images at HathiTrust)
• Langley Research Center: An evaluation of superminicomputers for thermal analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Olaf O. Storaasli, Gary K. Jones, James B. Vidal, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Goddard Space Flight Center (page images at HathiTrust)
• Langley Research Center: Evaluation of the influence of load randomization and of ground-air-ground cycles on fatigue life (National Aeronautics and Space Administration, 1964), also by Eugene C. Naumann and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Evaluation of the present theoretical basis for determination of planetary surface properties by earth-based radar (National Aeronautics and Space Administration ;, 1975), also by Leo D. Staton (page images at HathiTrust)
• Langley Research Center: Evaluation of the thin deformable active optics mirror concept (National Aeronautics and Space Administration ;, 1972), also by Hugh J. Robertson and Perkin-Elmer Corporation. Optical Group (page images at HathiTrust)
• Langley Research Center: Evaluation of turbulence reduction devices for the Langley 8-foot Transonic Pressure Tunnel (National Aeronautics and Space Administration, 1981), also by Marion O. McKinney, James Scheiman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Evaluation of two transport aircraft and several ground test vehicle friction measurements obtained for various runway surface types and conditions : a summary of test results from Joint FAA/NASA Runway Friction Program (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Thomas J. Yager, Paul Baldasare, William A. Vogler, and Joint FAA/NASA Runway Friction Program (page images at HathiTrust)
• Langley Research Center: Evaluation of vacuum UV detector-spectroscopy systems for capsule reentry measurements (National Aeronautics and Space Administration ;, 1969), also by Ronald L. Ohlhaber, H. V. Watts, M. W. Cann, IIT Research Institute, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Evaluation of verification and testing tools for FORTRAN programs (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Kathryn A. Smith and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Evaluation of wet tantalum capacitors after exposure to extended periods of ripple current. Volume II (National Aeronautics and Space Administration ;, 1975), also by C. M. Ward and Martin Marietta Aerospace. Denver Division (page images at HathiTrust)
• Langley Research Center: Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by L. Tracy Redd, Eleanor C. Wynne, Perry W. Hanson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Evidence of the beam pattern concept of subsonic jet noise emission (National Aeronautics and Space Administration ;, 1976), also by S. Paul Pao and Lucio Maestrello (page images at HathiTrust)
• Langley Research Center: An examination of methods of buffeting analysis based on experiments with wings of varying stiffness (National Aeronautics and Space Administration, 1959), also by A. Gerald Rainey and Thomas A. Byrdsong (page images at HathiTrust)
• Langley Research Center: Examination of onboard training for extended space flights (National Aeronautics and Space Administration :, 1964), also by Richard Reid and Rayford T. Saucer (page images at HathiTrust)
• Langley Research Center: Excess noise in tunable diode lasers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Carroll W. Rowland and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Exhaust-nozzle characteristics for a twin-jet variable-wing-sweep fighter airplane model at Mach numbers to 2.2 (National Aeronautics and Space Administration ;, 1974), also by David E. Reubush and Charles E. Mercer (page images at HathiTrust)
• Langley Research Center: Expanded operational capabilities of the Langley Mach 7 scramjet test facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Scott R. Thomas, Robert W. Guy, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experimenmtal flutter results for corrugation-stiffened and unstiffened panels (National Aeronautics and Space Administration ;, 1966), also by Deene J. Weidman (page images at HathiTrust)
• Langley Research Center: Experimental aerodynamic characteristics at Mach numbers from 0.60 to 2.70 of two supersonic cruise fighter configurations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Samuel M. Dollyhigh and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Experimental aerodynamic heating of simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Don E. Avery (page images at HathiTrust)
• Langley Research Center: Experimental and analytical determination of vibration characteristics of corrugated, flexibly supported, heat-shield panels (National Aeronautics and Space Administration ;, 1974), also by Huey D. Carden (page images at HathiTrust)
• Langley Research Center: Experimental and analytical investigation of axisymmetric supersonic cruise nozzle geometry at Mach numbers form 0.60 to 1.30 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by George T. Carson, Edwin E. Lee, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An experimental and analytical investigation of the effect on isolated boattail drag of varying Reynolds number up to 130 x 106 (National Aeronautics and Space Administration ;, 1976), also by David E. Reubush, Lawrence E. Putnam, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Experimental and analytical studies of advanced air cushion landing systems (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by E. G. S. Lee, Foster-Miller Associates, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experimental and analytical study of an inlet forebody for an airframe-integrated scramjet concept (National Aeronautics and Space Administration ;, 1975), also by Earl H. Andrews, S. Z. Pinckney, and Anthony M. Agnone (page images at HathiTrust)
• Langley Research Center: An experimental and analytical study of the aerodynamic interference effects between two Sears-Haack bodies at Mach 2.7 (National Aeronautics and Space Administration ;, 1985), also by Jeffrey W. Bantle (page images at HathiTrust)
• Langley Research Center: Experimental and analytical study of the longitudinal aerodynamic characteristics of analytically and empirically designed strake-wing confirurations at subcritical speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John E. Lamar, Neal T. Frink, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experimental and analytical transonic flutter characteristics of a geared-elevator configuration (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Charles L. Ruhlin, Richard A. Gregory, Robert V. Doggett, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Experimental and calculated supersonic flutter characteristics of models of the x-15 horizontal and vertical tails (National Aeronautics and Space Administration, 1959), also by William T. Lauten, R. W. Hess, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Experimental and numerical investigation of boundary-layer development and transition on the walls of a Mach 5 nozzle (National Aeronautics and Space Administration ;, 1975), also by William D. Harvey, Julius E. Harris, and Aubrey M. Cary (page images at HathiTrust)
• Langley Research Center: Experimental and predicted heating distributions for biconics at incidence in air at Mach 10 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Charles G. Miller (page images at HathiTrust)
• Langley Research Center: Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Zachary T. Applin and Garl L. Gentry (page images at HathiTrust)
• Langley Research Center: Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Jimmy L. Pittman, Gregory D. Riebe, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An experimental and theoretical investigation of plane-stress fracture of 2024-T351 aluminum alloy (National Aeronautics and Space Administration ;, 1970), also by C. E. Feddersen and Battelle Memorial Institute. Columbus Laboratories (page images at HathiTrust)
• Langley Research Center: Experimental and theoretical investigation of the ablative performance of five phenolic-nylon-based materials (National Aeronautics and Space Administration ;, 1968), also by Allen G. McLain, Gerald D. Walberg, and Kenneth Sutton (page images at HathiTrust)
• Langley Research Center: Experimental and theoretical low-speed aerodynamic characteristics of the NACA 65₁-213, a = 0.50 airfoil (National Aeronautics and Space Administration ;, 1975), also by William D. Beasley and William D. McGhee (page images at HathiTrust)
• Langley Research Center: Experimental and theoretical studies of axisymmetric free jets (U.S. G.P.O., 1959), also by Eugene S. Love and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Experimental and theoretical study of three interacting, closely-spaced, sharp-edged 60⁰ delta wings at low speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by H. F. Faery, J. A. Ham, J. K. Strozier, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and United States Military Academy. Dept. of Mechanics (page images at HathiTrust)
• Langley Research Center: Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Milton Lamb, James L. Thomas, Wallace C. Sawyer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experimental assessment of a computer program used in space shuttle orbiter entry heating analyses (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by William L. Wells, JoAnn Hudgins, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experimental atmospheric absorption values from aircraft flyover noise signals (National Aeronautics and Space Administration, 1971), also by Dwight E. Bishop, Myles A. Simpson, David T. Chang, United States National Aeronautics and Space Administration, and Beranek Bolt (page images at HathiTrust)
• Langley Research Center: Experimental behavior of graphite-epoxy Y-stiffened specimens loaded in compression (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by P. Daniel Sydow and Mark J. Shuart (page images at HathiTrust)
• Langley Research Center: Experimental boundary-layer edge Mach numbers for two space shuttle orbiters at hypersonic speeds (National Aeronautics and Space Administration, 1972), also by George C. Ashby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Experimental cavity pressure distributions at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Robert L. Stallings and Floyd J. Wilcox (page images at HathiTrust)
• Langley Research Center: Experimental data on single-bolt joints in quasi-isotropic graphite/polyimide laminates (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982), also by Gregory R. Wichorek and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experimental data on stagnation-point gas injection cooling on a hemisphere-cone in a hypersonic arc tunnel (National Aeronautics and Space Administration ;, 1964), also by John E. Grimaud and Leonard C. McRee (page images at HathiTrust)
• Langley Research Center: The experimental determination of atmospheric absorption from aircraft acoustic flight tests (National Aeronautics and Space Administration :, 1971), also by R. L. Miller, P. B. Oncley, United States National Aeronautics and Space Administration, and Boeing Company (page images at HathiTrust)
• Langley Research Center: Experimental determination of flow-interference effects of wing-mounted two-dimensional, full-capture propulsion nacelles in close proximity to a vehicle body at a Mach number of 6 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Walter A. Vahl and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experimental determination of position-estimate accuracy using back-azimuth signals from a microwave landing system (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1979), also by Charles E. Knox and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60 degree delta-wing airplane model (National Aeronautics and Space Administration, 1960), also by Lewis R. Fisher (page images at HathiTrust)
• Langley Research Center: Experimental determination of the effects of moisture on composite-to-composite adhesive joints (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Richard J. DeIasi, Robert L. Schulte, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experimental effects of fuselage camber on longitudinal aerodynamic characteristics of a series of wing-fuselage configurations at a mach of 1.41 (U.S. National Aeronautics and Space Administration ;, 1976), also by Samuel M. Dollyhigh, Mary S. Adams, Odell A. Morris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Experimental evaluation of 3 types of thermal protection materials at moderate heating rates and high total heat loads (National Aeronautics and Space Administration, 1963), also by Andrew J. Chapman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Experimental evaluation of a pilot multinozzle-duct apparatus (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Richard L. Puster and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Experimental evaluation of joint designs for a space-shuttle orbiter ablative leading edge (National Aeronautics and Space Administration ;, 1975), also by Stephen S. Tompkins and Walter P. Kabana (page images at HathiTrust)
• Langley Research Center: An experimental feasibility study for the preparation of thermo-oxidatively stable Pyrrone laminates (National Aeronautics and Space Administration ;, 1969), also by H. R. Lubowitz and TRW Systems Group (page images at HathiTrust)
• Langley Research Center: Experimental heat-transfer distributions on a blunt lifting body at Mach 3.71 (National Aeronautics and Space Administration ;, 1970), also by Robert L. Stallings, Ida K. Collins, Robert L. Wright, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Experimental investigation at a Mach number of 3.11 of the lift, drag, and pitching-moment characteristics of five blunt lifting bodies (National Aeronautics and Space Administration, 1960), also by William Letko (page images at HathiTrust)
• Langley Research Center: An experimental investigation at a Mach number of 4.95 of flow in the vicinity of a 90 degree interior corner alined with the free-stream velocity (National Aeronautics and Space Administration, 1960), also by P. Calvin Stainback (page images at HathiTrust)
• Langley Research Center: Experimental investigation at Mach 8 of the effects of projections and cavities on heat transfer to a model of the Viking aeroshell (National Aeronautics and Space Administration ;, 1974), also by Theodore R. Creel (page images at HathiTrust)
• Langley Research Center: An experimental investigation of a cold jet emitting from a body of revolution into a subsonic free stream (National Aeronautics and Space Administration ;, 1972), also by Donald Stewart Ousterhout and Old Dominion University. Research Foundation (page images at HathiTrust)
• Langley Research Center: Experimental investigation of a double-diffused MOS structure (U.S. National Aeronautics and Space Administration ;, 1976), also by Hung Chang Lin, J. L. Halsor, United States National Aeronautics and Space Administration, and Westinghouse Defense and Electronics Systems Center (page images at HathiTrust)
• Langley Research Center: An experimental investigation of a highly underexpanded sonic jet ejecting from a flat plate into a subsonic crossflow (National Aeronautics and Space Administration ;, 1973), also by Craig S. Shaw, Richard J. Margason, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An experimental investigation of a large [Delta]P settling chamber for a supersonic pilot quiet tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1981), also by Michael J. Piatt, Systems and Applied Sciences Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experimental investigation of a Mach 6 fixed-geometry inlet featuring a swept external-internal compression flow field (National Aeronautics and Space Administration ;, 1975), also by Marvin G. Torrence (page images at HathiTrust)
• Langley Research Center: Experimental investigation of a plasma-covered cavity-backed slot antenna (National Aeronautics and Space Administration ;, 1969), also by Thomas G. Campbell, William F. Croswell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Experimental investigation of a swept-strut fuel-injector concept for scramjet application (National Aeronautics and Space Administration ;, 1977), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics (National Aeronautics and Space Administration, 1959), also by Robert V. Doggett, Homer G. Morgan, and A. Gerald Rainey (page images at HathiTrust)
• Langley Research Center: An experimental investigation of an advanced turboprop installation on a swept wing at subsonic and transonic speeds (National Aeronautics and Space Administration Scientific and Technical Information Office ;, 1987), also by John R. Carlson and Odis C. Pendergraft (page images at HathiTrust)
• Langley Research Center: Experimental investigation of base heating and rocket hinge moments for a simulated missile through a Mach number range of 0.8 to 2.0 (National Aeronautics and Space Administration, 1959), also by Bruce G. Chiccine, Arthur M. Shinn, and Alfred S. Valerino (page images at HathiTrust)
• Langley Research Center: An experimental investigation of base heating on typical Mars entry body shapes (National Aeronautics and Space Administration ;, 1971), also by O. L. Zappa, William G. Reinecke, and Avco Corporation. Systems Division (page images at HathiTrust)
• Langley Research Center: An experimental investigation of dynamic ground effect (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987), also by Pai Hung Lee, Vincent U. Muirhead, and C. Edward Lan (page images at HathiTrust)
• Langley Research Center: Experimental investigation of effect of jet decay rate on jet-induced pressures on a flat plate (National Aeronautics and Space Administration, Scientfic and Technical Information Office ;, 1978), also by John M. Kuhlman, Ronald W. Warcup, Don S. Ousterhout, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Experimental investigation of jet impingement on surfaces of fine particles in a vacuum environment (National Aeronautics and Space Administration :, 1965), also by Norman S. Land and Leonard V. Clark (page images at HathiTrust)
• Langley Research Center: Experimental investigation of model variable-geometry and ogee tip rotors (National Aeronautics and Space Administration ;, 1974), also by Anton J. Landgrebe, E. Dean Bellinger, and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
• Langley Research Center: Experimental investigation of orthotropic panel flutter at arbitrary yaw angles, and comparison with theory (National Aeronautics and Space Administration ;, 1973), also by Peter Shyprykevich and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Experimental investigation of packaging and deployment characteristics of an inflatable toroidal-space-station configuration (National Aeronautics and Space Administration ;, 1965), also by Clarence O. Keffer (page images at HathiTrust)
• Langley Research Center: Experimental investigation of porous-floor effects on cavity flow fields at supersonic speeds (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Floyd J. Wilcox (page images at HathiTrust)
• Langley Research Center: An experimental investigation of the aerodynamics and cooling of a horizontally-opposed air-cooled aircraft engine installation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Stan J. Miley and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experimental investigation of the cornering characteristics of 18 x 5.5, type VII, aircraft tires with different tread patterns (National Aeronautics and Space Administration ;, 1974), also by Robert C. Dreher and John A. Tanner (page images at HathiTrust)
• Langley Research Center: Experimental investigation of the cornering characteristics of a C40 x 14-21 cantilever aircraft tire (National Aeronautics and Space Administration ;, 1972), also by Robert C. Dreher and John A. Tanner (page images at HathiTrust)
• Langley Research Center: An experimental investigation of the damping contribution of an elastomeric ablator on aluminum beams (National Aeronautics and Space Administration ;, 1974), also by William E. Howell (page images at HathiTrust)
• Langley Research Center: Experimental investigation of the effect of aspect ratio and Mach number on the flutter of cantilever wings (National Aeronautics and Space Administration, 1960), also by E. Widmayer, S. A. Clevenston, and W. T. Lauten (page images at HathiTrust)
• Langley Research Center: Experimental investigation of the effect of model scale on structural-joint damping (National Aeronautics and Space Administration ;, 1967), also by David G. Stephens, Maurice A. Scavullo, and Brantley R. Hanks (page images at HathiTrust)
• Langley Research Center: Experimental investigation of the effects of compressive stress on the flutter of a curved panel and a flat panel at supersonic Mach numbers (National Aeronautics and Space Administration, 1962), also by R. W. Hess, Frederick W. Gibson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Experimental investigation of the landing dynamics of three-legged spacecraft models (National Aeronautics and Space Administration ;, 1974), also by Sandy M. Stubbs (page images at HathiTrust)
• Langley Research Center: Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine (National Aeronautics and Space Administration, 1959), also by Thomas P. Moffitt and Frederick W. Klag (page images at HathiTrust)
• Langley Research Center: Experimental investigation of the pressure fluctuations on a flat plate and a cylinder in the slipstream of a hovering rotor (National Aeronautics and Space Administration, 1959), also by John W. McKee (page images at HathiTrust)
• Langley Research Center: Experimental investigation of the transonic flutter of simple thin truncated-cone panels (National Aeronautics and Space Administration, 1961), also by Jean Gilman (page images at HathiTrust)
• Langley Research Center: An experimental investigation of thrust vectoring two-dimensional covergent-divergent nozzles installed in a twin-engine fighter model at high angles of attack (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Francis J. Capone, Laurence D. Leavitt, and Mary L. Mason (page images at HathiTrust)
• Langley Research Center: An experimental investigation of two visual methods of altitude determination (National Aeronautics and Space Administration ;, 1967), also by Jacob H. Lichtenstein and William T. Suit (page images at HathiTrust)
• Langley Research Center: An experimental investigation of vortex generation in a turbulent boundary layer undergoing adverse pressure gradient (National Aeronautics and Space Administration ;, 1972), also by Victor Zakkay, Wladimiro Calarese, and New York University (page images at HathiTrust)
• Langley Research Center: An experimental investigation of vortex stability, tip shapes, compressibility, and noise for hovering model rotors (National Aeronautics and Space Administration ;, 1973), also by James L. Tangler, Stan J. Miley, Robert M. Wohlfeld, and Bell Helicopter Company (page images at HathiTrust)
• Langley Research Center: An experimental investigation of wall boundary-layer transition Reynolds numbers in an expansion tube (National Aeronautics and Space Administration ;, 1974), also by K. James Weilmuenster (page images at HathiTrust)
• Langley Research Center: Experimental investigation to determine utility of tension shell concept (National Aeronautics and Space Administration ;, 1966), also by W. Jefferson Stroud and George W. Zender (page images at HathiTrust)
• Langley Research Center: Experimental investigation to validate use of cryogenic temperatures to achieve high Reynolds numbers in boattail pressure testing (U.S. National Aeronautics and Space Administration ;, 1976), also by David E. Reubush and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing (National Aeronautics and Space Administration ;, 1974), also by Jim A. Penland, Floyd G. Howard, and Theodore R. Creel (page images at HathiTrust)
• Langley Research Center: Experimental operating performance of a single-stage annular air ejector (National Aeronautics and Space Administration, 1959), also by Robert R. Howell (page images at HathiTrust)
• Langley Research Center: Experimental parametric studies of transonic T-tail flutter (National Aeronautics and Space Administration ;, 1975), also by Charles L. Ruhlin and M. C. Sandford (page images at HathiTrust)
• Langley Research Center: Experimental perfect-gas study of expansion-tube flow characteristics (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Judy L. Shinn, Charles G. Miller, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Experimental performance of an ablative material as an external insulator for a hpersonic research aircraft (National Aeronautics and Space Administration ;, 1977), also by Richard L. Puster, Andrew J. Chapman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Experimental performance of an internal resistance heater for Langley 6-inch expansion tube driver (National Aeronautics and Space Administration ;, 1972), also by Thomas R. Creel (page images at HathiTrust)
• Langley Research Center: Experimental performance of liquid hydrogen and liquid fluorine in regeneratively cooled rocket engines (National Aeronautics and Space Administration, 1959), also by H. W. Douglass, H. G. Price, and G. Hennings (page images at HathiTrust)
• Langley Research Center: Experimental plasma studies (National Aeronautics and Space Administration ;, 1972), also by M. G. Dunn and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Langley Research Center: An experimental pressure-distribution investigation of interference effects produced at a Mach number of 3.11 by wedge- shaped bodies located under a triangular wing (National Aeronautics and Space Administration, 1959), also by Lowell E. Hasel (page images at HathiTrust)
• Langley Research Center: Experimental separation studies for two-dimensional wedges and curved surfaces at Mach numbers of 4.8 to 6.2 (National Aeronautics and Space Administration, 1962), also by James R. Sterrett and James C. Emery (page images at HathiTrust)
• Langley Research Center: An experimental simulation study of four crosswind landing-gear concepts (National Aeronautics and Space Administration ;, 1975), also by Sandy M. Stubbs, Robert K. Sleeper, and Thomas A. Byrdsong (page images at HathiTrust)
• Langley Research Center: Experimental stability and control results at Mach 19 of an entry vehicle designed for an intermediate lift-drag ratio (National Aeronautics and Space Administration ;, 1968), also by Patrick J. Johnston and Robert D. Witcofski (page images at HathiTrust)
• Langley Research Center: Experimental studies for determining human discomfort response to vertical sinusoidal vibration (National Aeronautics and Space Administration ;, 1975), also by Thomas K. Dempsey and Jack D. Leatherwood (page images at HathiTrust)
• Langley Research Center: Experimental studies of flow separation and stalling on a two-dimensional airfoil at low speeds (National Aeronautics and Space Administration, 1975), also by H. C. Seetharam, W. H. Wentz, and Wichita State University (page images at HathiTrust)
• Langley Research Center: Experimental studies of hypersonic boundary-layer transition and effects of wind-tunnel disturbances (National Aeronautics and Space Administration ;, 1974), also by P. Calvin Stainback (page images at HathiTrust)
• Langley Research Center: Experimental studies on the aerodynamic performance and dynamic response of flow direction sensing vanes (National Aeronautics and Space Administration ;, 1976), also by P.S. Barna, Gary R. Crossman, United States National Aeronautics and Space Administration, and Old Dominion University (page images at HathiTrust)
• Langley Research Center: Experimental study in vacuum of the rate-of-rise outgassing-measurement technique (National Aeronautics and Space Administration ;, 1969), also by Gerald L. Gregory and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Experimental study of a free turbulent shear flow at Mach 19 with electron-beam and conventional probes (National Aeronautics and Space Administration ;, 1975), also by William D. Harvey and William W. Hunter (page images at HathiTrust)
• Langley Research Center: Experimental study of a hot structure for a reentry vehicle (National Aeronautics and Space Administration, 1961), also by Richard A. Pride, Bobbie F. Helms, and Dick M. Royster (page images at HathiTrust; US access only)
• Langley Research Center: Experimental study of a single-coil induced-electromotive-force plasma accelerator (National Aeronautics and Space Administration, 1961), also by Clarence W. Matthews and William F. Cuddihy (page images at HathiTrust)
• Langley Research Center: Experimental study of acoustic loads on upper-surface-blown STOL airplane configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Conrad M. Willis, James A. Schoenster, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experimental study of cluster formation in binary mixture of H₂0 and H₂S0₄ vapors in the presence of an ionizing radiation source (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Jag J. Singh, Glenn K. Yue, Alphonso C. Smith, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An experimental study of continuous plasma flows driven by a confined arc in a transverse magnetic field (National Aeronautics and Space Administration, 1961), also by Raymond L. Barger, William D. Beasley, and Joseph D. Brooks (page images at HathiTrust)
• Langley Research Center: Experimental study of low-energy charge transfer in nitrogen (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Alphonso C. Smith and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experimental study of noise reduction for an unstiffened cylindrical model of an airplane fuselage (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Conrad M. Willis, Edward F. Daniels, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An experimental study of rotor blade-vortex interaction (National Aeronautics and Space Administration, 1970), also by Makam Surendraiah, United States National Aeronautics and Space Administration, and Pennsylvania State University (page images at HathiTrust)
• Langley Research Center: Experimental study of rotor unsteady airloads due to blade-vortex interaction (National Aeronautics and Space Administration, 1971), also by Raghuveera Padakannaya, United States National Aeronautics and Space Administration, and Pennsylvania State University (page images at HathiTrust)
• Langley Research Center: Experimental study of sharp- and blunt-nose streamwise corners at Mach 20 (National Aeronautics and Space Administration ;, 1974), also by Ralph D. Watson (page images at HathiTrust)
• Langley Research Center: An experimental study of slot injection into a supersonic stream (National Aeronautics and Space Administration ;, 1973), also by Michael Kenworthy, Joseph A. Schetz, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Langley Research Center: Experimental study of the effects of installation on single- and counter-rotation propeller noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by P. J. W. Block (page images at HathiTrust)
• Langley Research Center: An experimental study of the flutter of sails having a delta planform tested from a Mach number of 0.1 to a Mach number of 1.9 (National Aeronautics and Space Administration, 1961), also by R. W. Hess and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An experimental study of the validity of the heat-field concept for sonic-boom alleviation (National Aeronautics and Space Administration ;, 1974), also by Rudolph J. Swigart and Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: An experimental study of tip shape effects on the flutter of aft-swept, flat-plate wings (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Bryan E. Dansberry, Moses G. Farmer, and Jose A. Rivera (page images at HathiTrust)
• Langley Research Center: Experimental study of transient effects in dielectric materials caused by electron irradiation (National Aeronautics and Space Administration ;, 1965), also by George M. Storti, Clifford S. Frank, and Donald H. Phillips (page images at HathiTrust)
• Langley Research Center: Experimental study of transmission and backscatter of 0.075 to 1.0 MeV electrons by aluminum and stainless steel (National Aeronautics and Space Administration ;, 1968), also by William E. Miller and Herbert D. Hendricks (page images at HathiTrust)
• Langley Research Center: Experimental uncertainty and drag measurements in the national transonic facility (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Stephen M. Batill (page images at HathiTrust)
• Langley Research Center: Experimental validation of a landing-dynamics computer program for legged spacecraft landers (National Aeronautics and Space Administration ;, 1973), also by John R. McGehee and Sandy M. Stubbs (page images at HathiTrust)
• Langley Research Center: Experimental validation of a two-dimensional shear-flow model for determining acoustic impedance (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Tony L. Parrott, Michael G. Jones, and Willie R. Watson (page images at HathiTrust)
• Langley Research Center: Experimental validation of clock synchronization algorithms (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Daniel L. Palumbo and R. Lynn Graham (page images at HathiTrust)
• Langley Research Center: An experimental wind-tunnel investigation of a ram-air-spoiler roll-control device on a forward-control missile at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by A. B. Blair and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Experiments in sensing transient rotational accelaration cues on a flight simulator (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Russell V. Parrish and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Experiments on the effects of atmospheric refraction and airplane accelerations on sonic-boom ground-pressure patterns (National Aeronautics and Space Administration, 1966), also by Domenic J. Maglieri, Norman J. McLeod, David A. Hilton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An explicit upwind algorithm for solving the parabolized Navier-Stokes equations (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by John J. Korte (page images at HathiTrust)
• Langley Research Center: Exploiting symmetries in the modeling and analysis of tires (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Ahmed Khairy Noor, John A. Tanner, and Carl M. Andersen (page images at HathiTrust)
• Langley Research Center: An Exploration of function analysis and function allocation in the commercial flight domain (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by James C. McGuire and Douglas Aircraft Company (page images at HathiTrust)
• Langley Research Center: Exploratory heat-transfer measurements at Mach 10 on a 7.5 ̊total-angle cone downstream of a region of air and helium transpiration cooling (National Aeronautics and Space Administration ;, 1969), also by James C. Dunavant, Philip E. Everhart, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An exploratory investigation of a transport configuration designed for supersonic cruise flight near a Mach number of 3 (National Aeronautics and Space Administration, 1960), also by Ausley B. Carraway, Melvin M. Carmel, and Donald T. Gregory (page images at HathiTrust)
• Langley Research Center: An exploratory investigation of a wake disruption technique for studying wake reestablishment time (National Aeronautics and Space Administration ;, 1974), also by Louis E. Clark and Robert A. Jones (page images at HathiTrust)
• Langley Research Center: Exploratory investigation of several coated and uncoated metal, refractory, and graphite models in a 3800° F stagnation temperature air jet (National Aeronautics and Space Administration, 1960), also by Otto F. Trout (page images at HathiTrust)
• Langley Research Center: Exploratory investigation of sound pressure level in the wake of an oscillating airfoil in the vicinity of stall (National Aeronautics and Space Administration ;, 1972), also by Robin B. Gray, G. A. Pierce, and Georgia Institute of Technology (page images at HathiTrust)
• Langley Research Center: Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Peter T. Bernot (page images at HathiTrust)
• Langley Research Center: Exploratory investigation of the effect of porous surfaces on hypersonic turbulent boundary layers (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Ralph D. Watson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: An exploratory investigation of the low-speed aerodynamic characteristics of variable-wing-sweep airplane configurations (National Aeronautics and Space Administration, 1959), also by Williams J. Alford, William P. Handerson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Exploratory investigation of two resin-matrix composites subjected to arc-tunnel heating (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by C. M. Pittman, Ronald D. Brown, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: An exploratory simulation study of a head-on display for general aviation lightplanes (National Aeronautics and Space Administration ;, 1973), also by Randall L. Harris and Donald E. Hewes (page images at HathiTrust)
• Langley Research Center: An exploratory study of a new class of stepladder and ladder polymers - polyimidazopyrrolones (National Aeronautics and Space Administration ;, 1965), also by George F. Pezdirtz and Vernon Lee Bell (page images at HathiTrust)
• Langley Research Center: Exploratory study of man's self locomotion capabilities with a space suit in lunar gravity (National Aeronautics and Space Administration ;, 1966), also by Amos A. Spady and William D. Krasnow (page images at HathiTrust)
• Langley Research Center: Exploratory study of the effects of wing-leading-edge modifications on the stall/spin behavior of a light general aviation airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Exploratory study of transient unstart phenomena in a three-dimensional fixed-geometry scramjet engine (U.S. National Aeronautics and Space Administration ;, 1976), also by Allan R. Wieting (page images at HathiTrust)
• Langley Research Center: Exploratory tests of two strut fuel injectors for supersonic combustion (National Aeronautics and Space Administration ;, 1974), also by Griffin Y. Anderson and Paul B. Gooderum (page images at HathiTrust)
• Langley Research Center: Exploratory wind-tunnel investigation of a wingtip-mounted vortex turbine for vortex energy recovery (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by James C. Patterson and Stuart G. Flechner (page images at HathiTrust)
• Langley Research Center: Exploratory wind-tunnel investigation of deployable flexible ventral fins for use as an emergency spin-recovery device (National Aeronautics and Space Administration, 1971), also by Sanger M. Burk and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An exploratory wind-tunnel investigation of the wake effect of a panel tip-mounted fan-jet engine on the lift-induced vortex (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1970), also by James C. Patterson, Stuart G. Flechner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The Explorer XXIII micrometeoroid satellite description and preliminary results for the period November 6, 1964 through February 15, 1965 (National Aeronautics and Space Administration ;, 1965), also by Robert L. O'Neal and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The Explorer XXIII micrometeoroid satellite : description and results for the period November 6, 1964, through November 5, 1965 (National Aeronautics and Space Administration ;, 1968), also by Robert L. O'Neal (page images at HathiTrust)
• Langley Research Center: Explosive and pyrotechnic aging demonstration (National Aeronautics and Space Administration ;, 1976), also by Lawrence L. Rouch, J. Norman Maycock, and Martin Marietta Laboratories (page images at HathiTrust)
• Langley Research Center: Extension of leading-edge-suction analogy to wings with separated flow around the side edges at subsonic speeds (National Aeronautics and Space Administration ;, 1974), also by John E. Lamar (page images at HathiTrust)
• Langley Research Center: An extension of the Laplace transform to Schwartz distributions (National Aeronautics and Space Administration, 1974), also by Douglas B. Price (page images at HathiTrust)
• Langley Research Center: An extension of the QZ algorithm for solving the generalized matrix eigenvalue problem (National Aeronautics and Space Administration ;, 1973), also by Robert C. Ward and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Extraction from flight data of lateral aerodynamic coefficients for F-8 aircraft with supercritical wing (National Aeronautics and Space Administration ;, 1974), also by James L. Williams and William T. Suit (page images at HathiTrust)
• Langley Research Center: Extraction from flight data of longitudinal aerodynamic coefficients for F-8 aircraft with supercritical wing (National Aeronautics and Space Administration ;, 1974), also by James L. Williams and William T. Suit (page images at HathiTrust)
• Langley Research Center: Extraction of longitudinal aerodynamic coefficients from forward-flight conditions of a tilt wing V/STOL airplane (National Aeronautics and Space Administration ;, 1972), also by James L. Williams and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An extremely thin, omnidirectional, microwave antenna array for spacecraft applications (National Aeronautics and Space Administration ;, 1969), also by Thomas G. Campbell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: F-15 rotary balance data for an angle-of-attack range of 8⁰ to 90⁰ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Billy Barnhart and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: F-8C adaptive flight control laws (National Aeronautics and Space Administration ;, 1977), also by Honeywell Systems and Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: F-8C digital CCV flight control laws (U.S. National Aeronautics and Space Administration ;, 1976), also by Gary L. Hartmann, Russell C. Hendrick, James A. Hauge, and Honeywell Systems and Research Center (page images at HathiTrust)
• Langley Research Center: FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance : proceedings of a symposium jointly sponsored by the Federal Aviation Administration, Washington, DC, and the National Aeronautics and Space Administration, Washington, DC, and held in Hampton, Virginia, May 4-6, 1994 (Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1994-, 1994), also by Va.) FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance (1994 : Hampton, Charles E. Harris, United States National Aeronautics and Space Administration, and United States Federal Aviation Administration (page images at HathiTrust)
• Langley Research Center: FAA/NASA Joint University Program for Air Transportation Research 1992-1993 : proceedings of a conference sponsored by the Federal Aviation Administration, Washington, D.C., and the National Aeronautics and Space Administration, Washington, D.C., and held in Athens, Ohio, June 17-18, 1993 (Langley Research Center, 1994), also by Frederick R. Morrell, United States National Aeronautics and Space Administration, and United States Federal Aviation Administration (page images at HathiTrust)
• Langley Research Center: Fabrication of photovoltaic laser energy converter by MBE (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), also by Hamilton Lu, Wen S. Chan, Scott Wang, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: Fail-safe system for actively cooled supersonic and hypersonic aircraft (National Aeronautics and Space Administration ;, 1975), also by Robert A. Jones, Christine B. Richie, and Dorothy O. Braswell (page images at HathiTrust)
• Langley Research Center: Failure analysis and mechanisms of failure of fibrous composite structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983), also by Ahmed Khairy Noor, Joint Institute for Advancement of Flight Sciences, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and George Washington University (page images at HathiTrust)
• Langley Research Center: Failure analysis of aluminum alloy components (National Aeronautics and Space Administration ;, 1973), also by Om Johari, Joseph Staschke, Irene Corvin, and IIT Research Institute (page images at HathiTrust)
• Langley Research Center: A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Pierce L. Lawing, Charles L. Ladson, Jerry B. Adcock, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A fast-acting electrical servo for the actuation of full-span, Fowler-type wing flaps in DLC applications : a detail design study / by Frederick O. Smetana, Rafael J. Montoya, and Ronald K. Carden. (National Aeronautics and Space Administration ;, 1972), also by Frederick O. Smetana, Ronald K. Carden, Rafael J. Montoya, and North Carolina State University (page images at HathiTrust)
• Langley Research Center: Fatigue-crack initiation and growth in notched 2024-T 3 specimens monitored by a video tape system (U.S. National Aeronautics and Space Administration ;, 1976), also by J. A. Sova, R. J. Exton, John H. Crews, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Fatigue-crack-propagation and fracture-toughness characteristics of 7079 aluminum-alloy sheets and plates in three aged conditions (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), also by S. H. Smith, W. D. Sump, T. R. Porter, and Boeing Company (page images at HathiTrust)
• Langley Research Center: Fatigue evaluation of composite-reinforced, integrally stiffened metal panels : summary (National Aeronautics and Space Administration ;, 1973), also by C. E. Dumesnil and Vought Aeronautics Company (page images at HathiTrust)
• Langley Research Center: Fatigue of four stainless steels, four titanium alloys, and two aluminum alloys before and after exposure to elevated temperatures for up to three years (National Aeronautics and Space Administration ;, 1971), also by Walter Illg, L. A. Imig, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Fatigue of notched Ti-8Al-1Mo-1V titanium alloy at room temperature and 550⁰ F (560⁰ K) with flight-by-flight loading representative of a supersonic transport (National Aeronautics and Space Administration ;, 1969), also by L. A. Imig, Walter Illg, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Fatigue-test acceleration with flight-by-flight loading and heating to simulate supersonic-transport operation (National Aeronautics and Space Administration ;, 1973), also by L. A. Imig and L. E. Garrett (page images at HathiTrust)
• Langley Research Center: Fatigue under random and programmed loads (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1965), also by Eugene C. Naumann and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Fault tolerance of artificial neural networks with applications in critical systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Peter W. Protzel, Michael K. Arras, and Daniel L. Palumbo (page images at HathiTrust)
• Langley Research Center: The Fault-Tree Compiler (FTC) : program and mathematics (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Ricky W. Butler and Anna L. Martensen (page images at HathiTrust)
• Langley Research Center: Feasibility breadboard of an all-magnetic PCM telemetry system (National Aeronautics and Space Administration ;, 1966), also by C. H. Heckler, J. A. Baer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations (National Aeronautics and Space Administration, Scientific and Technical Information Service ;, 1979), also by D. Brooke, D. V. Vondrasek, McDonnell Douglas Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A feasibility study for Scout polar launches from NASA Wallops Flight Center (National Aeronautics and Space Administration ;, 1975), also by T. R. Myler and LTV Aerospace Corporation. Vought Systems Division (page images at HathiTrust)
• Langley Research Center: Feasibility study of a low-energy gamma ray system for measuring quantity and flow rate of slush hydrogen (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Jag J. Singh, Danny R. Sprinkle, and Chih-Ping Shen (page images at HathiTrust)
• Langley Research Center: A feasibility study of a miniature solid-state pressure transducer (National Aeronautics and Space Administration ;, 1969), also by C. D. Parker and Research Triangle Institute (page images at HathiTrust)
• Langley Research Center: A feasibility study of determining physical properties of the Martian atmosphere by use of solar occultation as seen from an artificial satellite (National Aeronautics and Space Administration ;, 1969), also by H. Andrew Wallio and James R. Williams (page images at HathiTrust)
• Langley Research Center: A feasibility study of heat-pipe-cooled leading edges for hypersonic cruise aircraft (National Aeronautics and Space Administration, 1971), also by Calvin C. Silverstein and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Feasibility study of shell buckling analysis using the modified structure method (National Aeronautics and Space Administration ;, 1972), also by Gerald A. Cohen, Raphael T. Haftka, and Structures Research Associates (page images at HathiTrust)
• Langley Research Center: Feasibility study on the development of tough, moisture-resistant laminating resins (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by R. A. Brand, E. S. Harrison, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Field test to intercompare carbon monoxide, nitric oxide, and hydroxyl instrumentation at Wallops Island, Virginia (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Gerald L. Gregory, Richard J. Bendura, and Sherwin M. Beck (page images at HathiTrust)
• Langley Research Center: A filter spectrometer concept for facsimile cameras (National Aeronautics and Space Administration ;, 1974), also by Daniel J. Jobson, Stephen D. Wall, and W. Lane Kelly (page images at HathiTrust)
• Langley Research Center: Finite deformation of elasto-plastic solids (National Aeronautics and Space Administration ;, 1973), also by J. R. Osias and Carnegie-Mellon University (page images at HathiTrust)
• Langley Research Center: A finite-difference analysis of the nozzle starting process in an expansion tunnel (National Aeronautics and Space Administration ;, 1975), also by K. James Weilmuenster (page images at HathiTrust)
• Langley Research Center: A finite-difference method for predicting supersonic turbulent boundary-layer flows with tangential slot injection (National Aeronautics and Space Administration, 1972), also by E. W. Miner, C. H. Lewis, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Langley Research Center: A finite difference method for the solution of the transonic flow around harmonically oscillating wings (National Aeronautics and Space Administration ;, 1974), also by F. Edward Ehlers and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Finite-difference solution of the compressible stability eigenvalue problem (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Mujeeb R. Malik, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Systems and Applied Sciences Corporation (page images at HathiTrust)
• Langley Research Center: Finite element analysis and computer graphics visualization of flow around pitching and plunging airfoils (National Aeronautics and Space Administration ;, 1973), also by Theodore Bratanow, Akin Ecer, and University of Wisconsin--Milwaukee (page images at HathiTrust)
• Langley Research Center: Finite-element-analysis model and preliminary ground testing of Controls-Structures Interaction Evolutionary Model reflector (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Mercedes C. Reaves, James P. Bailey, and W. Keith Belvin (page images at HathiTrust)
• Langley Research Center: Finite element analysis of aeroacoustic jet-flap flows (Nat'l Aeronautics & Space Admin., Scientific & Technical Information Office ;, 1977), also by A. J. Baker, P. D. Manhardt, Computational Mechanics Consultants, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A finite element for thermal stress analysis of shells of revolution (National Aeronautics and Space Administration ;, 1973), also by Howard M. Adelman, James L. Rogers, and Harold C. Lester (page images at HathiTrust)
• Langley Research Center: Finite geometry corrections to gamma-ray angular correlation measurements (National Aeronautics and Space Administration :, 1965), also by Jag J. Singh and Chris Gross (page images at HathiTrust)
• Langley Research Center: First derivatives of flow quantities behind two-dimensional, nonuniform supersonic flow over a convex corner (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Christine M. Darden (page images at HathiTrust)
• Langley Research Center: First evaluation of the main parameters in the dynamics of the Small Expendable Deployer System (SEDS) for a tethered satellite (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by L. De Luca and Joint Institute for Advancement of Flight Sciences (page images at HathiTrust)
• Langley Research Center: First-order optical analysis of a quasi-microscope for planetary landers (National Aeronautics and Space Administration ;, 1973), also by Friedrich O. Huck, Ernest E. Burcher, Archibald R. Sinclair, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Fixed-base simulation study of a pilot's ability to control a winged-satellite vehicle during high-drag variable-lift entries (National Aeronautics and Space Administration, 1960), also by John M. Eggleston, Donald C. Cheatham, and Sheldon Baron (page images at HathiTrust)
• Langley Research Center: Fixed-base simulation study of decoupled longitudinal controls during approach and landing of a medium jet transport in the presence of wind shear (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by G. Kimball Miller and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Fixed-base simulator study of the effect of time delays in visual cues on pilot tracking performance (National Aeronautics and Space Administration ;, 1975), also by M. J. Queijo and Donald R. Riley (page images at HathiTrust)
• Langley Research Center: Fixed-base visual simulation of pilot controlled descents of an advanced Apollo spacecraft with an all-flexible parawing (National Aeronautics and Space Administration ;, 1969), also by G. Kimball Miller, Douglas B. Price, and Byron M. Jacquet (page images at HathiTrust)
• Langley Research Center: FLEXAN (version 2.0) user's guide (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1989), also by Scott S. Stallcup (page images at HathiTrust)
• Langley Research Center: Flight and ground tests of a very-low-density elastomeric ablative material (National Aeronautics and Space Administration ;, 1972), also by George C. Olsen and Andrew Chapman (page images at HathiTrust)
• Langley Research Center: Flight assessment of a large supersonic drone aircraft for research use (National Aeronautics and Space Administration ;, 1975), also by Clinton V. Eckstrom and Ellwood L. Peele (page images at HathiTrust)
• Langley Research Center: Flight assessment of an atmospheric turbulence measurement system with emphasis on long wavelengths (National Aeronautics and Space Administration ;, 1976), also by Richard H. Rhyne (page images at HathiTrust)
• Langley Research Center: Flight deck benefits of integrated data link communication (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Marvin C. Waller (page images at HathiTrust)
• Langley Research Center: Flight demonstration of a nose-mounted rotating-solid-propellant rocket control system and a comparison with analog studies (National Aeronautics and Space Administration ;, 1966), also by Kirby H. Williams and Robert L. James (page images at HathiTrust)
• Langley Research Center: Flight effects of fan noise : proceedings of a workshop held at Langley Research Center (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A Flight evaluation of a vectored-thrust-jet V/STOL airplane during simulated instrument approaches using the Kestrel (XV-6A) airplane (National Aeronautics and Space Administration ;, 1972), also by Samuel A. Morello, Richard G. Culpepper, Robert E. Shanks, Lee H. Person, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A flight evaluation of a VTOL jet transport under visual and simulated instrument conditions (National Aeronautics and Space Administration, 1972), also by Curt A. Holzhauser, James M. Patton, Robert C. Innis, Samuel A. Morello, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Flight instrument and telemetry response and its inversion (National Aeronautics and Space Administration, 1971), also by M. R. Weinberger, Avco Corporation. Systems Division, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Flight investigation of a capacitance-type meteoroid detector using an inflatable paraglider (National Aeronautics and Space Administration ;, 1968), also by James H. Siviter and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Flight investigation of a centrally located rigid force control stick used with electronic control systems in a fighter airplane (National Aeronautics and Space Administration, 1959), also by Walter R. Russell and William L. Alford (page images at HathiTrust)
• Langley Research Center: Flight investigation of a solar orientation control system for spacecraft (National Aeronautics and Space Administration , 1964), also by Anthony Fontana (page images at HathiTrust)
• Langley Research Center: Flight investigation of a V/STOL transport model with four pod-mounted lift fans (National Aeronautics and Space Administration, 1971), also by William A. Newsom, Sue B. Grafton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Flight investigation of a vertical-velocity command system for VTOL aircraft (National Aeronautics and Space Administration ;, 1977), also by James R. Kelly and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A flight investigation of an acceleration restrictor (National Aeronautics and Space Administration, 1960), also by Arthur Assadourian and Donald L. Mallick (page images at HathiTrust)
• Langley Research Center: Flight investigation of an automatic pitchup control (National Aeronautics and Space Administration, 1960), also by George J. Hurt and James B. Whitten (page images at HathiTrust)
• Langley Research Center: Flight investigation of cockpit-displayed traffic information utilizing coded symbology in an advanced operational environment (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Terence S. Abbott, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings (National Aeronautics and Space Administration ;, 1974), also by James R. Kelly (page images at HathiTrust)
• Langley Research Center: A flight investigation of piloting techniques and crosswind limitations during visual STOL-Type landing operations (National Aeronautics and Space Administration ;, 1976), also by Bruce D. Fisher and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Flight investigation of piloting techniques and crosswind limitations using a research-type crosswind land gear (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office and Bruce D. Fisher (page images at HathiTrust)
• Langley Research Center: Flight investigation of stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane (National Aeronautics and Space Administration, 1960), also by Louis P. Tosti (page images at HathiTrust)
• Langley Research Center: Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by H. Paul Stough, James M. Patton, and Daniel J. DiCarlo (page images at HathiTrust)
• Langley Research Center: Flight investigation of steep instrument approach capabilities of a T-33 airplane under manual control (National Aeronautics and Space Administration ;, 1965), also by Albert W. Hall and Donald J. McGinley (page images at HathiTrust)
• Langley Research Center: Flight investigation of the effects of an outboard wing-leading-edge modification on stall/spin characteristics of a low-wing, single-engine, T-tail light airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by H. Paul Stough, James M. Patton, and Daniel J. DiCarlo (page images at HathiTrust)
• Langley Research Center: A flight investigation of the trailing vortices generated by a jumbo jet transport (National Aeronautics and Space Administration ;, 1973), also by Harry A. Verstynen and R. Earl Dunham (page images at HathiTrust)
• Langley Research Center: Flight investigation of the VFR and IFR landing approach characteristics and terminal area airspace requirements for a light STOL airplane (National Aeronautics and Space Administration ;, 1974), also by Harold L. Crane, Bruce D. Fisher, and Kenneth R. Yenni (page images at HathiTrust)
• Langley Research Center: Flight investigation of V/STOL height-control requirements for hovering and low-speed flight under visual conditions (National Aeronautics and Space Administration, 1967), also by James R. Kelly, Perry L. Deal, and John F. Garren (page images at HathiTrust)
• Langley Research Center: A Flight investigation with STOL airplane flying curved, descending instrument approach paths (National Aeronautics and Space Administration ;, 1974), also by Margaret S. Benner (page images at HathiTrust)
• Langley Research Center: Flight investigations of automatic stabilization of an airplane having static longitudinal instability (National Aeronautics and Space Administration, 1959), also by Walter R. Russell, William L. Alford, and S. A. Sjoberg (page images at HathiTrust)
• Langley Research Center: Flight loads measurements obtained from calibrated strain-gage bridges mounted externally on the skin of a low-aspect-ratio wing (National Aeronautics and Space Administration ;, 1976), also by Clinton V. Eckstrom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Flight-measured laminar boundary layer transition phenomena including stability theory analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Clifford J. Obara and Bruce J. Holmes (page images at HathiTrust)
• Langley Research Center: A flight measurement of optical radiation from shock-heated air by using a Trailblazer II vehicle (National Aeronautics and Space Administration ;, 1968), also by Lloyd S. Keafer, Ernest E. Burcher, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Flight measurements of surface pressures on a flexible supercritical research wing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Clinton V. Eckstrom (page images at HathiTrust)
• Langley Research Center: Flight measurements of the effects of blade out of track on the vibration levels on a tandem rotor helicopter (National Aeronautics and Space Administration, 1960), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Flight technology improvement : proceedings of a workshop sponsored jointly by the Office of Aeronautics and Space Technology and the Office of Space and Terrestrial Applications of NASA Headquarters and the NASA Langley Research Center, and held at College Park, Maryland, July 31-August 2, 1979. (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1979), also by Flight Technology Improvement Workshop (1979 : University of Maryland) and United States. Office of Aeronautics and Space Technology (page images at HathiTrust)
• Langley Research Center: Flight test data for a Cessna Cardinal (National Aeronautics and Space Administration ;, 1974), also by David L. Kohlman and University of Kansas. Center for Research (page images at HathiTrust)
• Langley Research Center: Flight test measurements and analysis of sonic boom phenomena near the shock wave extremity (National Aeronautics and Space Administration ;, 1973), also by George T. Haglund, Edward J. Kane, and Boeing Company (page images at HathiTrust)
• Langley Research Center: Flight test of a 15-foot-diameter (4.6-meter) 120 ̊conical spacecraft simulating parachute deployment in a Mars atmosphere (National Aeronautics and Space Administration ;, 1967), also by Wayne L. Darnell, Reginald R. Lundstrom, and Allen B. Henning (page images at HathiTrust)
• Langley Research Center: Flight test of a 30-foot nominal diameter disk-gap-band parachute deployed at a Mach number of 1.56 and a dynamic pressure of 11.4 pounds per square foot (National Aeronautics and Space Administration ;, 1967), also by Clinton V. Eckstrom and John S. Preisser (page images at HathiTrust)
• Langley Research Center: Flight test of a 31.2-foot-diameter modified ringsail parachute deployed at a Mach number of 1.39 and a dynamic pressure of 11.0 pounds per square foot (National Aeronautics and Space Administration, 1967), also by John S. Preisser, Harold N. Murrow, and Clinton V. Eckstrom (page images at HathiTrust)
• Langley Research Center: Flight test of a Little Joe boosted full-scale spacecraft model and escape system for Project Mercury (National Aeronautics and Space Administration, 1962), also by Hal T. Baber, Roland D. English, and Howard S. Carter (page images at HathiTrust)
• Langley Research Center: Flight test of a pitch control for a spinning vehicle (National Aeronautics and Space Administration, 1963), also by H. Douglas Garner and H. J. E. Reid (page images at HathiTrust)
• Langley Research Center: Flight test of a pure-tone acoustic source (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Arnold W. Mueller, John S. Preisser, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Flight test of an erectable spacecraft used for decelerator testing at simulated Mars entry conditions (National Aeronautics and Space Administration ;, 1972), also by Allen B. Henning and Reginald R. Lundstrom (page images at HathiTrust)
• Langley Research Center: Flight test performance and description of a rocket vehicle for producing low-speed artificial meteors (National Aeronautics and Space Administration :, 1964), also by Clarence A. Brown and Jean C. Keating (page images at HathiTrust)
• Langley Research Center: Flight-test verification of a pictorial display for general aviation instrument approach (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), also by James J. Adams and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Flight testing techniques for the evaluation of light aircraft stability derivitives : a review and analysis (National Aeronautics and Space Administration, 1972), also by Frederick O. Smetana, W. Donald Johnson, Delbert C. Summey, United States National Aeronautics and Space Administration, and North Carolina State University (page images at HathiTrust)
• Langley Research Center: Flight tests of Viking parachute system in three Mach number regimes (National Aeronautics and Space Administration ;, 1974), also by Reginald R. Lundstrom (page images at HathiTrust)
• Langley Research Center: Flight tests with a data link used for air traffic control information exchange (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Charles E. Knox and Charles H. Scanlon (page images at HathiTrust)
• Langley Research Center: Flight transition data for angles of attack at Mach 22 with correlations of the data (National Aeronautics and Space Administration ;, 1975), also by Charles B. Johnson and Christine M. Darden (page images at HathiTrust)
• Langley Research Center: Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Oktay Baysal and Old Dominion University. Dept. of Mechanical Engineering and Mechanics (page images at HathiTrust)
• Langley Research Center: Flow field analysis of aircraft configurations using a numerical solution to the three-dimensional unified supersonic/hypersonic small disturbance equations (National Aeronautics and Space Administration ;, 1972), also by R. C. Gunness, E. Dsylva, C. J. Knight, and Boeing Company (page images at HathiTrust)
• Langley Research Center: Flow-field measurements around a Mars lander model using hot-film anemometers under simulated Mars surface conditions (National Aeronautics and Space Administration ;, 1972), also by George C. Greene (page images at HathiTrust)
• Langley Research Center: Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by E. Ann Bare, Raymond C. Haddad, and David E. Reubush (page images at HathiTrust)
• Langley Research Center: Flow separation in shock wave boundary layer interactions at hypersonic speeds (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by A. Hamed and Joint Institute for Advancement of Flight Sciences (page images at HathiTrust)
• Langley Research Center: Flow visualization and laser velocimetry for wind tunnels : proceedings of a NASA workshop held at Langley Research Center, Hampton, Virginia, March 25-26, 1982 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Jerome T. Foughner, William W. Hunter, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Workshop on Flow Visualization and Laser Velocimetry for Wind Tunnels (1982 : Langley Research Center) (page images at HathiTrust)
• Langley Research Center: Flow visualization by elastic light scattering in the boundary layer of a supersonic flow (National Aeronautics and Space Administration, Langley Research Center, 2000), also by G. C. Herring and Mervin E. Hillard (page images at HathiTrust)
• Langley Research Center: Flow visualization in a cryogenic wind tunnel using holography (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Alpheus W. Burner, William K. Goad, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Flow visualization studies of a general research fighter model employing a strake-wing concept at subsonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by James M. Luckring and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Flow visualization studies of blowing from the tip of a swept wing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Jeannette W. Smith, Dan H. Neuhart, and Raymond E. Mineck (page images at HathiTrust)
• Langley Research Center: Fluctuating loads measured on an over-the-wing supersonic jet model (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Conrad M. Willis and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Fluctuating pressures measured beneath a high-temperature, turbulent boundary layer on a flat plate at a Mach number of 5 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Tony L. Parrott, Cindy W. Albertson, and Michael G. Jones (page images at HathiTrust)
• Langley Research Center: Fluctuating pressures on fan blades of a turbofan engine : flight test investigation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by James A. Schoenster (page images at HathiTrust)
• Langley Research Center: Fluctuating pressures on fan blades of a turbofan engine : static and wind-tunnel investigations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by James A. Schonester and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Fluctuating surface pressure and acoustic radiation for subsonic normal jet impingement (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by John S. Preisser and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Fluctuating surface-pressure characteristics on slender cones in subsonic, supersonic, and hypersonic Mach-number flow (National Aeronautics and Space Administration ;, 1974), also by H. Heller, Anthony R. Clemente, and Beranek Bolt (page images at HathiTrust)
• Langley Research Center: Flush-mounted antennas radiating on aircraft type surfaces (National Aeronautics and Space Administration ;, 1974), also by Walter D. Burnside, R. J. Marhefka, C. L. Yu, and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: Flutter analysis and testing of pairs of aerodynamically interfering delta wings (National Aeronautics and Space Administration ;, 1973), also by Richard R. Chipman, Frank J. Rauch, and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Flutter analysis of an airplane with multiple structural nonlinearities in the control system (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Elmar J. Breitbach and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings (National Aeronautics and Space Administration ;, 1974), also by Jerrold M. Housner and Manuel Stein (page images at HathiTrust)
• Langley Research Center: Flutter at very high speeds (National Aeronautics and Space Administration, 1961), also by Harry L. Runyan, Homer G. Morgan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Flutter of a low-aspect-ratio rectangular wing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Stanley R. Cole (page images at HathiTrust)
• Langley Research Center: Flutter of elastically supported orthotropic panels including the effects of flow angle (National Aeronautics and Space Administration ;, 1974), also by James Wayne Sawyer (page images at HathiTrust)
• Langley Research Center: Flutter of panels on discrete flexible supports (National Aeronautics and Space Administration ;, 1974), also by Manuel Stein (page images at HathiTrust)
• Langley Research Center: Flutter Research on skin panels (National Aeronautics and Space Administration :, 1960), also by Eldon E. Kordes, Lawrence D. Guy, and W. J. Tuovila (page images at HathiTrust)
• Langley Research Center: Flutter suppression using active controls based on the concept of aerodynamic energy (National Aeronautics and Space Administration ;, 1971), also by E. Nissim and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Flyover noise characteristics of tilt-wing V/Stol aircraft (XC-142A) (National Aeronautics and Space Administration ;, 1974), also by Robert J. Pegg, David A. Hilton, and Herbert R. Henderson (page images at HathiTrust)
• Langley Research Center: The foot-controlled maneuvering unit : summary report on Skylab experiment T-020 (National Aeronautics and Space Administration ;, 1975), also by Donald E. Hewes and Kenneth E. Glover (page images at HathiTrust)
• Langley Research Center: Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Robert L. Calloway and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Force-penetration characteristics of a sand horizontally penetrated by plates, cones, and spherical segments (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1969), also by Paul A. Hustad, William Roy Cox, and University of Texas (page images at HathiTrust; US access only)
• Langley Research Center: Force-test investigation of the stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane (National Aeronautics and Space Administration, 1960), also by Louis P. Tosti (page images at HathiTrust)
• Langley Research Center: Fore-and-aft elastic response characteristics of 34 x 9.9, type VII, 14 ply-rating aircraft tires of bias-ply, bias-belted, and radial-belted design (National Aeronautics and Space Administration ;, 1974), also by John A. Tanner (page images at HathiTrust)
• Langley Research Center: Formal and heuristic system decomposition methods in multidisciplinary synthesis (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Christina L. Bloebaum and Mechanics University of Florida. Dept. of Aerospace Engineering (page images at HathiTrust)
• Langley Research Center: Formal methods and digital systems validation for airborne systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), also by John Rushby and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: A formal model of asynchronous communication and its use in mechanically verifying a biphase mark prorocol (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by J Strother Moore and Inc Computational Logic (page images at HathiTrust)
• Langley Research Center: Formal specification and verification of a fault-masking and transient-recovery model for digital flight-control systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by John Rushby and SRI International (page images at HathiTrust)
• Langley Research Center: Formal verification of a fault tolerant clock synchronization algorithm (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by John Rushby, Frieder von Henke, and SRI International (page images at HathiTrust)
• Langley Research Center: Formal verification of a microcoded VIPER microprocessor using HOL (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), also by Karl Levitt and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: A formally verified algorithm for interactive consistency under a hybrid fault model (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), also by Patrick Lincoln, John Rushby, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: Formulation of the information capacity of the optical-mechanical line-scan imaging process (National Aeronautics and Space Administration ;, 1975), also by Friedrich O. Huck and Stephen Keith Park (page images at HathiTrust)
• Langley Research Center: Formulation on statistical trajectory estimation programs (National Aeronautics and Space Administration ;, 1970), also by William E. Wagner, Arno C. Serold, and Martin Marietta Corporation (page images at HathiTrust)
• Langley Research Center: Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Michael J. Mann and Charles E. Mercer (page images at HathiTrust)
• Langley Research Center: A four-channel portable solar radiometer for measuring particulate and/or aerosol opacity and concentration of NO₂ and SO₂ in stack plumes (National Aeronautics and Space Administration ;, 1976), also by Reginald J. Exton and Ray W. Gregory (page images at HathiTrust)
• Langley Research Center: Four dimensional derivation of the electrodynamic jump conditions, tractions, and power transfer at a moving boundary (National Aeronautics and Space Administration :, 1965), also by Robert C. Costen (page images at HathiTrust)
• Langley Research Center: Four-engine turbojet transport airplane ... (National Aeronautics and Space Administration, 1970), also by Paul A. Hunter, Mary W. Fetner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Four microsecond flashing light synchronized with framing of motion-picture cameras and its application in Schlieren photography (National Aeronautics and Space Administration :, 1970), also by Walter F. Lindsey, Joseph Burlock, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Fracture behavior of thick, laminated graphite/epoxy composites (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), also by Charles E. Harris, D. H. Morris, Virginia Polytechnic Institute and State University, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Fracture toughness of boron/aluminum laminates with various proportions of 0° and ±45 ̊plies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by C. C. Poe, J. A. Sova, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Free drifting buoys : AIAA Drift Buoy Symposium, Hampton, Va., May 22-23, 1974 (NASA ;, 1976), also by Va.) AIAA Drift Buoy Symposium (1974 : Hampton and American Institute of Aeronautics and Astronautics. Technical Committee on Marine Systems and Technologies (page images at HathiTrust)
• Langley Research Center: Free-flight and wind-tunnel studies of deployment of a dynamically and elastically scaled inflatable parawing model (National Aeronautics and Space Administration ;, 1968), also by Alice T. Ferris, H. Neale Kelly, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Free-flight investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on an 80° delta-wing missile (National Aeronautics and Space Administration, 1960), also by Eugene D. Schult (page images at HathiTrust)
• Langley Research Center: Free-flight investigation of heat transfer to an unswept cylinder subjected to an incident shock and flow interference from an upstream body at Mach numbers up to 5.50 (National Aeronautics and Space Administration, 1961), also by Howard S. Carter, Robert E. Carr, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Free-flight investigation of the stability and control characteristics of a STOL model with an externally blown jet flap (National Aeronautics and Space Administration ;, 1974), also by Lysle P. Parlett, Arthur E. Phelps, and Sandy J. Emerling (page images at HathiTrust)
• Langley Research Center: Free-flight model investigation of a vertical-attitude VTOL fighter (National Aeronautics and Space Administration ;, 1975), also by William A. Newsom and Ernie L. Anglin (page images at HathiTrust)
• Langley Research Center: Free-stream electron concentration in an arc-heated wind tunnel and correlation of Langmuir probe and microwave interferometer measurements (National Aeronautics and Space Administration ;, 1969), also by Roy James Duckett and William Linwood Jones (page images at HathiTrust)
• Langley Research Center: Free vibrations of thermally stressed orthotropic plates with various boundary conditions (National Aeronautics and Space Administration ;, 1973), also by C. D. Bailey, James C. Greetham, and Ohio State University. Research Foundation (page images at HathiTrust)
• Langley Research Center: Free vibrations of thin-walled semicircular graphite-epoxy composite frames (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Ahmed Khairy Noor, Jeanne M. Peters, and Huey D. Carden (page images at HathiTrust)
• Langley Research Center: Free volume variation with molecular weight of polymers (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Jag J. Singh (page images at HathiTrust)
• Langley Research Center: FREQ : a computational package for multivariable system loop-shaping procedures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Daniel P. Giesy and Ernest S. Armstrong (page images at HathiTrust)
• Langley Research Center: Frequency domain laser velocimeter signal processor : a new signal processing scheme (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by James F. Meyers and James I. Clemmons (page images at HathiTrust)
• Langley Research Center: Frequency of encounter of aircraft in a random horizontal field (U.S. National Aeronautics and Space Administration, Langley Research Center ;, 1976), also by John D. Bird, Kathryn A. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Friction and wear characteristics of wire-brush skids (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Robert C. Dreher and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Friction characteristics of 20 x 4.4, type VII, aircraft tires constructed with different tread rubber compounds (U.S. National Aeronautics and Space Administration ;, 1976), also by Robert C. Dreher, Thomas J. Yager, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Full-coverage film cooling : 3-dimensional measurements of turbulence structure and prediction of recovery region hydrodynamics (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by S. Yavuzkurt, W. M. Kays, R. J. Moffat, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Full scale crash test evaluation of two load-limiting subfloors for general aviation airframes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Huey D. Carden (page images at HathiTrust)
• Langley Research Center: Full-scale dynamic landing-impact investigation of a prototype lunar module landing gear (National Aeronautics and Space Administration ;, 1969), also by Ulysse J. Blanchard and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Full-scale flight test from sea level of an abort-escape system for a Project Mercury capsule (National Aeronautics and Space Administration, 1960), also by Willard S. Blanchard and James L. Raper (page images at HathiTrust)
• Langley Research Center: Full-scale flight test of a proposed abort-escape system for a manned space capsule from sea level (National Aeronautics and Space Administration, 1960), also by Willard S. Blanchard and Sherwood Hoffman (page images at HathiTrust)
• Langley Research Center: Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by David E. Hahne and Frank L. Jordan (page images at HathiTrust)
• Langley Research Center: Full-scale wind-tunnel investigation of the low-speed static aerodynamic characteristics of a model of a reentry capsule (National Aeronautics and Space Administration, 1959), also by William I. Scallion (page images at HathiTrust)
• Langley Research Center: Full-scale wind-tunnel investigation on effects of slot spoilers on the aerodynamic characteristics of a light twin-engine airplane (National Aeronautics and Space Administration ;, 1973), also by Harry A. Verstynen, Dominick Andrisani, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Full-scale wind tunnel tests of a low-wing, single-engine, light plane with positive and negative propeller thrust and up and down flap deflection (National Aeronautics and Space Administration, 1971), also by Edward Seckel, United States National Aeronautics and Space Administration, and Princeton University (page images at HathiTrust)
• Langley Research Center: Fully-coupled analysis of jet mixing problems : three-dimensional PNS model, SCIP3D (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by D. E. Wolf, Sanford M. Dash, and N. Sinha (page images at HathiTrust)
• Langley Research Center: Fundamental mechanisms of tensile fracture in aluminum sheet unidirectionally reinforced with boron filament (National Aeronautics and Space Administration ;, 1972), also by Harvey W. Herring (page images at HathiTrust)
• Langley Research Center: Further analysis of broadband noise measurements for a rotating blade operating with and without its shed wake blown downstream (National Aeronautics and Space Administration ;, 1974), also by James Scheiman (page images at HathiTrust)
• Langley Research Center: Fuselage and nozzle pressure distributions on a 1/12-scale F-15 propulsion model at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Odis C. Pendergraft and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Fuselage design for a specified Mach-sliced area distribution (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Raymond L. Barger and Mary S. Adams (page images at HathiTrust)
• Langley Research Center: Future orbital transfer vehicle technology study (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), also by Eldon E. Davis, Boeing Aerospace Company, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: GaA1As/GaAs solar cell process study (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by David W. Almgren, Katinka I. Csigi, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: GEMPAK : an arbitrary aircraft geometry generator (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Sharon H. Stack, William J. Small, C. L. W. Edwards, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A general algorithm for relating ground trajectory distance, elapsed flight time, and aircraft airspeed and its application to 4-D guidance (National Aeronautics and Space Administration ;, 1975), also by Edwin C. Foudriat (page images at HathiTrust)
• Langley Research Center: General-aviation pilot reactions to and opinions on grooved runways (National Aeronautics and Space Administration ;, 1969), also by George E. Cranston and Flight Safety Foundation (page images at HathiTrust)
• Langley Research Center: A general aviation simulator evaluation of a rate-enhanced instrument landing system display (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by David A. Hinton and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A general form of the co-moving tensorial derivative (National Aeronautics and Space Administration ;, 1974), also by Earle K. Huckins and Richard E. Turner (page images at HathiTrust)
• Langley Research Center: A general method for calculating three-dimensional compressible laminar and turbulent boundary layers on arbitrary wings (National Aeronautics and Space Administration ;, 1977), also by Tuncer Cebeci, Judy A. Ramsey, Kalle Kaups, McDonnell Douglas Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A general method for designing circular array antennas to obtain quasi-omnidirectional patterns (National Aeronautics and Space Administration ;, 1967), also by C. R. Cockrell and W. F. Croswell (page images at HathiTrust)
• Langley Research Center: A general review of concepts for reducing skin friction, including recommendations for future studies (National Aeronautics and Space Administration ;, 1974), also by Michael C. Fischer and Robert L. Ash (page images at HathiTrust)
• Langley Research Center: A general theory of unsteady compressible potential aerodynamics (National Aeronautics and Space Administration ;, 1974), also by L. Morino and Boston University. College of Engineering (page images at HathiTrust)
• Langley Research Center: A generalized chemistry version of SPARK (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Mark H. Carpenter (page images at HathiTrust)
• Langley Research Center: Generalized hypercube structures and hyperswitch communication network (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Steven D. Young (page images at HathiTrust)
• Langley Research Center: A generalized vortex lattlice method for subsonic and supersonic flow applications (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Luis R. Miranda, William M. Baker, Robert D. Elliott, Lockheed-California Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Generation of X-rays and neutrons with a RF-discharge (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Richard T. Schneider, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and RTS Laboratories (page images at HathiTrust)
• Langley Research Center: Geometric, aerodynamic, and kinematic characteristics of two twin keel parawings during deployment (National Aeronautics and Space Administration ;, 1971), also by Paul M. Kenner, Ralph B. Holt, Frederic T. Churchill, United States National Aeronautics and Space Administration, and Vought Missiles and Space Division LTV Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Geometric modeling and analysis of large latticed surfaces (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1980), also by Adnan H. Nayfeh, Mohamed S. Hefzy, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Geometric relationships for homogenization in single-phase binary alloy systems (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Jalaiah Unnam, Bland A. Stein, Darrel R. Tenney, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Joint Institute for Advancement of Flight Sciences (page images at HathiTrust)
• Langley Research Center: A geometry package for generation of input data for a three-dimensional potenial-flow program (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by N. Douglas Halsey, John L. Hess, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Gigaflop performance on a CRAY-2 : multitasking a computational fluid dynamics application (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Geoffrey M. Tennille (page images at HathiTrust)
• Langley Research Center: GIM code user's manual for the STAR-100 computer (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1979), also by Lawrence Spradley, Mark Pearson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Gladstone-Dale constant for CF4 / Alpheus W. Burner, Jr., and William K. Goad. (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1980), also by Alpheus W. Burner and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A global search and rescue concept using synthetic aperture radar and passive user targets (U.S. National Aeronautics and Space Administration ;, 1976), also by W. E. Sivertson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Godunov method and computer program to determine the pressure and flow field associated with a sonic boom focus (National Aeronautics and Space Administration ;, 1973), also by Lee W. Parker, Robert G. Zalosh, and Mass.) Mt. Auburn Associates (Somerville (page images at HathiTrust)
• Langley Research Center: Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Ivan E. Beckwith, Barbara B. Holley, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Graphical workstation capability for reliability modeling (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Salvatore J. Bavuso, Pamela J. Haley, and Sandra V. Koppen (page images at HathiTrust)
• Langley Research Center: Graphite/Polyimide composites (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by John G. Davis, H. Benson Dexter, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and CASTS Project Technical Symposium (1979 : Langley Research Center) (page images at HathiTrust)
• Langley Research Center: Gravitational experiments with a collisionless two-dimensional computer model (National Aeronautics and Space Administration ;, 1968), also by Frank Hohl, Stephen K. Park, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The gravitational field environment of an earth satellite (National Aeronautics and Space Administration, 1962), also by David Adamson (page images at HathiTrust)
• Langley Research Center: Grid generation and flow solution method for Euler equations on unstructured grids (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by W. Kyle Anderson (page images at HathiTrust)
• Langley Research Center: Grid systems for earth radiation budget experiment applications (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by David R. Brooks and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Ground-based and in-flight simulator studies of flight characteristics of a twin-fuselage passenger transport airplane during approach and landing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by William D. Grantham (page images at HathiTrust)
• Langley Research Center: Ground effect for lifting rotors in forward flight (National Aeronautics and Space Administration, 1960), also by Harry H. Heyson (page images at HathiTrust)
• Langley Research Center: Ground effects on the low-speed aerodynamics of a powered, generic hypersonic configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Gregory M. Gatlin (page images at HathiTrust)
• Langley Research Center: Ground measurements of airplane shock-wave noise at Mach numbers to 2.0 and at altitudes to 60,000 feet (National Aeronautics and Space Administration, 1960), also by Lindsay J. Lina and Domenic J. Maglieri (page images at HathiTrust)
• Langley Research Center: Ground measurements of sonic-boom pressures for the altitude range of 10,000 to 75,000 feet (National Aeronautics and Space Administration :, 1964), also by Harvey H. Hubbard and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Ground measurements of the shock-wave noise from airplanes in level flight at Mach numbers to 1.4 and at altitudes to 45,000 feet (National Aeronautics and Space Administration, 1959), also by Domenic J. Maglieri, Donald L. Lansing, and Harvey H. Hubbard (page images at HathiTrust)
• Langley Research Center: Ground noise measurements during landing, take-off, and flyby operations of a four-engine turbopropeller STOL airplane (National Aeronautics and Space Administration ;, 1971), also by David A. Hilton, Domenic J. Maglieri, Herbert R. Henderson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Ground vibration test of an F-16 airplane with modified decoupler pylons (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by F. W. Cazier and M. W. Kehoe (page images at HathiTrust)
• Langley Research Center: Ground vibration test of the laminar flow control JetStar airplane (National Aeronautics and Space Administration, Scientific and Technical Branch ;, 1985), also by M. W. Kehoe, Joseph F. Ellison, and F. W. Cazier (page images at HathiTrust)
• Langley Research Center: Growth of high-quality thin-film Ge single crystals by plasma-enhanced chemical vapor deposition (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by R. A. Outlaw and P. Hopson (page images at HathiTrust)
• Langley Research Center: Growth of surface and corner cracks in beta-processed and mill-annealed Ti-6Al-4V (National Aeronautics and Space Administration ;, 1975), also by Paul D. Bell (page images at HathiTrust)
• Langley Research Center: Grumman H-33 space shuttle orbiter aerodynamic and handling-qualities study (National Aeronautics and Space Administration ;, 1972), also by Robert W. Rainey (page images at HathiTrust)
• Langley Research Center: Guidance and control during direct-descent parabolic reentry (National Aeronautics and Space Administration, 1961), also by Edwin C. Foudriat, Rodney C. Wingrove, United States National Aeronautics and Space Administration, Ames Research Center, and D.C.) NASA-Industry Apollo Technical Conference (1961 : Washington (page images at HathiTrust)
• Langley Research Center: Guidance, navigation, and control susbsystem equipment selection algorithm using expert system methods (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Cheryl L. Allen (page images at HathiTrust)
• Langley Research Center: Guide for users of the National Transonic Facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Dennis E. Fuller and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Guide to Lunar Orbiter photographs (Scientific and Technical Information Office, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U. S. Govt. Print. Off.], 1971), also by Thomas P. Hansen (page images at HathiTrust)
• Langley Research Center: A guide to the use of the pressure disk rotor model as implemented in INS3D-UP (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by Mark S. Chaffin and Inc ViGYAN (page images at HathiTrust)
• Langley Research Center: Guidelines for composite materials research related to general aviation aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Norris F. Dow, E. A. Humphreys, B. W. Rosen, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Materials Sciences Corporation (page images at HathiTrust)
• Langley Research Center: Gust alleviation for a STOL transport by using elevator, spoilers, and flaps (National Aeronautics and Space Administration ;, 1974), also by Frederick J. Lallman (page images at HathiTrust)
• Langley Research Center: HADY-1, a FORTRAN program for the compressible stability analysis of three-dimensional boundary layers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Nabil M. El-Hady and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A handbook for the estimation of airside delays at major airports (quick approximation method) (U.S. National Aeronautics and Space Administration ;, 1976), also by Amedeo R. Odoni, Peeter Andrus Kivestu, Massachusetts Institute of Technology. Flight Transportation Laboratory, United States Federal Aviation Administration, United States. Dept. of Transportation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Handbook of aircraft noise metrics (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Ricarda L. Bennett and Karl S. Pearsons (page images at HathiTrust)
• Langley Research Center: A harmonic analysis method for unsteady transonic flow and its application to the flutter of airfoils (National Aeronautical and Space Administration, Scientific and Technical Information Branch ;, 1982), also by F. Edward Ehlers, W. H. Weatherill, Boeing Commercial Airplane Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Heat generation in aircraft tires under braked rolling conditions (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), also by Samuel K. Clark, Richard N. Dodge, and University of Michigan. Dept. of Mechanical Engineering & Applied Mechanics (page images at HathiTrust)
• Langley Research Center: Heat generation in aircraft tires under free rolling conditions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Samuel K. Clark, Richard N. Dodge, University of Michigan. Dept. of Mechanical Engineering, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Heat-transfer and pressure distributions for laminar separated flows downstream of rearward-facing steps with and without mass suction (National Aeronautics and Space Administration ;, 1974), also by Ronald D. Brown and Antoni K. Jakubowski (page images at HathiTrust)
• Langley Research Center: Heat-transfer and pressure distributions on hemisphere-cylinders in methane-air combustion products at Mach 7 (National Aeronautics and Space Administration ;, 1973), also by Irving Weinstein and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Heat-transfer and pressure measurements on a concove-nose cylinder for a mach number range of 2.49 to 4.44 (National Aeronautics and Space Administration, 1959), also by Jr. Stallings and Paige B. Burbank (page images at HathiTrust)
• Langley Research Center: Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at Mach 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Charles B. Johnson, Louis G. Kàufman, Grumman Aerospace Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0 ̊to 180 ̊ (National Aeronautics and Space Administration ;, 1976), also by Milton Lamb, Robert L. Stallings, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Heat-transfer measurements at a Mach number of 2 in the turbulent boundary layer on a flat plate having a stepwise temperature distribution (National Aeronautics and Space Administration, 1959), also by Raul J. Conti (page images at HathiTrust)
• Langley Research Center: Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 (National Aeronautics and Space Administration, 1959), also by Charles B. Rumsey and Dorothy B. Lee (page images at HathiTrust)
• Langley Research Center: Heat-transfer measurements on a low-fineness-ratio cylinder at a mach number of 10.4 and angles of attack from 0 degree to 90 degress (National Aeronautics and Space Administration ;, 1967), also by Philip E. Everhart (page images at HathiTrust)
• Langley Research Center: Heat-transfer tests of 20-millimeter projectiles at a Mach number of 5 with an analysis by unsteady scaling laws to predict component temperature rises after firing for various free-flight conditions (National Aeronautics and Space Administration, 1961), also by Robert L. Trimpi, Robert A. Jones, and James G. Gallagher (page images at HathiTrust)
• Langley Research Center: Helicopter acoustics : proceedings of an International Specialists Symposium sponsored by the American Helicopter Society, Washington, D.C.; the U.S. Army Research Office, Durham, North Carolina; and the Langley Research Center, Hampton, Virginia, and held at Langley Research Center, May 22-24, 1978. (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by International Specialists Symposium on Helicopter Acoustics (1978 : Langley Research Center), American Helicopter Society, and N.C.) United States. Army Research Office (Durham (page images at HathiTrust)
• Langley Research Center: Helicopter rotor rotational noise predictions based on measured high-frequency blade loads (National Aeronautics and Space Administration ;, 1974), also by Robert N. Hosier and Ramani Ramakrishnan (page images at HathiTrust)
• Langley Research Center: Helicopter rotor trailing edge noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Robert H. Schlinker, Roy K. Amiet, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Helicopter vibration suppression using simple pendulum absorbers on the rotor blade (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by G. Alvin Pierce, M-Nabil H. Hamouda, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Helium concentrations downstream of a vent exhausting helium at sonic velocity into a supersonic stream of air at Mach numbers of 3.51 and 4.50 (National Aeronautics and Space Administration, 1963), also by Robert L. Stallings, Paul W. Howard, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: A Hierarchy of transport approximations for high energy heavy (HZE) ions (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by John W. Wilson (page images at HathiTrust)
• Langley Research Center: High-altitude flight test of a 40-foot-diameter (12.2-meter) ringsail parachute at a deployment Mach number of 2.95 (National Aeronautics and Space Administration, 1970), also by Clinton V. Eckstrom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: High-altitude flight test of a reefed 12.2-meter-diameter disk-gap-band parachute with deployment at a mach number of 2.58 (National Aeronautics and Space Administration :, 1971), also by John S. Preisser, R. Bruce Grow, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: High energy proton radiation damage to (AlGa)As--GaAs solar cells (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by R. Loo and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A high frequency correction to the Kirchoff approximation with application to rough surface EM wave scattering (New York University, School of Engineering and Science, Dept. of Meteorology and Oceanography, in the 1970s), also by Frederick C. Jackson and New York University. School of Engineering and Science (page images at HathiTrust)
• Langley Research Center: High heat flux actively cooled honeycomb sandwich structural panel for a hypersonic aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by L. C. Koch, L. L. Pagel, McDonnell Douglas Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: High L/D concept with single pivot two position skewed wing (National Aeronautics and Space Administration ;, 1970), also by B. J. Kuchta and General Dynamics Corporation (page images at HathiTrust)
• Langley Research Center: High-lift characteristics of a variable-sweep supersonic transport model with a blended engine-fuselage and engine-mounted horizontal tails (National Aeronautics and Space Administration ;, 1966), also by Vernard E. Lockwood (page images at HathiTrust)
• Langley Research Center: A high-performance 250-pound-thrust rocket engine utilizing coaxial-flow injection of JP-4 fuel and liquid oxygen (National Aeronautics and Space Administration, 1959), also by Samuel Stein (page images at HathiTrust)
• Langley Research Center: High performance, accelerometer-based control of the mini-MAST structure at Langley Research Center (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Emmanuel G. Collins and Harris Corporation. Government Aerospace Systems Division (page images at HathiTrust)
• Langley Research Center: High performance S-band horn antennas for radiometer use (National Aeronautics and Space Administration ;, 1973), also by R. Caldecott and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: A high-presure premixed flat-flame burner for chemical process studies (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Irvin M. Miller and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: The High Resolution Accelerometer Package (HiRAP) flight experiment summary for the first 10 flights (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Robert C. Blanchard, K. T. Larman, and M. Barrett (page images at HathiTrust)
• Langley Research Center: High resolution infrared spectroscopy techniques for upper atmospheric measurements : proceedings of a workshop sponsored by the National Aeronautics and Space Administration, and held at Silverthorne, Colorado, July 31-August 2, 1979 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by J. M. Alvarez, D. G. Murcray, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: High Reynolds number test of a NACA 65₁-213, a = 0.5 airfoil at transonic speeds (National Aeronautics and Space Administration ;, 1975), also by Kenneth P. Burdges, Gerald A. Pounds, James A. Blackwell, and Lockheed-Georgia Company (page images at HathiTrust)
• Langley Research Center: High Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by William G. Johnson, Otto Eichmann, and Acquilla S. Hill (page images at HathiTrust)
• Langley Research Center: High-speed assembly language (80386/80387) programming for laser spectra scan control and data acquisition providing improved resolution water vapor spectroscopy (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Robert J. Allen, Vigyan Research Associates, and Allen Associates (page images at HathiTrust)
• Langley Research Center: High-speed civil transport study (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Boeing Commercial Airplane Company. New Airplane Development Group (page images at HathiTrust)
• Langley Research Center: High-speed flow past wings (National Aeronautics and Space Administration ;, 1973), also by Helge Nørstrud and Lockheed-Georgia Company (page images at HathiTrust)
• Langley Research Center: High speed lookup table approach to radiometric calibration of multispectral image data (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by W. Lane Kelly, Barry D. Meredith, William M. Howle, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0 degree to 90 degree (National Aeronautics and Space Administration, 1959), also by Bernard Spencer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A high subsonic speed wind-tunnel investigation of winglets on a representative second-generation jet transport wing (National Aeronautics and Space Administration ;, 1976), also by Stuart G. Flechner, Richard T. Whitcomb, Peter F. Jacobs, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: High-temperature chemical kinetic study of the H₂-CO-CO₂-NO reaction system (National Aeronautics and Space Administration ;, 1975), also by Casimir J. Jachimowski (page images at HathiTrust)
• Langley Research Center: High-temperature dielectric properties of candidate space-shuttle thermal-protection-system and antenna-window materials (National Aeronautics and Space Administration ;, 1974), also by Melvin C. Gilreath and Stark L. Castellow (page images at HathiTrust)
• Langley Research Center: Higher-order numerical methods derived from three-point polynomial interpolation (National Aeronautics and Space Administration ;, 1976), also by Stanley G. Rubin, Prem K. Khosla, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Langley Research Center: Higher-order numerical solutions using cubic splines (U.S. National Aeronautics and Space Administration, Langley Research Center ;, 1976), also by S. G. Rubin, P. K. Khosla, and New York (State). Polytechnic Institute (page images at HathiTrust)
• Langley Research Center: Historical perspectives on thermostructural research at the NACA Langley Aeronautical Laboratory from 1948 to 1958 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Richard R. Heldenfels and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Holographic and ultrasonic detection of bond flaws in aluminum panels reinforced with boron-epoxy (National Aeronautics and Space Administration ;, 1974), also by Robert J. Platt and Lewis B. Thurston (page images at HathiTrust)
• Langley Research Center: Holographic flow visualization at the Langley Expansion Tube (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by William K. Goad, Alpheus W. Burner, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Holographic measurement of wave propagation in axi-symmetric shells (National Aeronautics and Space Administration ;, 1972), also by David A. Evensen, Jerold L. Jacoby, Robert Aprahamian, and TRW Systems Group (page images at HathiTrust)
• Langley Research Center: Homing performance comparison of selected airframe configurations using skid-to-turn and bank-to-turn steering policies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by R. T. Reichert, Johns Hopkins University, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Hot-salt-stress-corrosion cracking and its effect on tensile and stress-rupture properties of Ti-6Al-4V titanium-alloy sheet (National Aeronautics and Space Administration ;, 1969), also by Dick M. Royster and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Hot-wire anemometry in hypersonic helium flow (National Aeronautics and Space Administration ;, 1974), also by Richard D. Wagner and Leonard M. Weinstein (page images at HathiTrust)
• Langley Research Center: Hover performance tests of full scale variable geometry rotors (U.S. National Aeronautics and Space Administration ;, 1976), also by James B. Rorke, United States National Aeronautics and Space Administration, United Technologies Corporation, and U.S. Army Air Mobility Research and Development Laboratory (page images at HathiTrust)
• Langley Research Center: How a pilot looks at altitude (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Amos A. Spady, Randall L. Harris, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Human discomfort response to noise combined with vertical vibration (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Jack D. Leatherwood and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A human operator simulator model of the NASA Terminal Configured Vehicle (TCV) (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Floyd A. Glenn and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Human transfer functions in multi-axis and multi-loop control systems (National Aeronautics and Space Administration ;, 1966), also by James J. Adams, George J. Hurt, and Hugh P. Bergeron (page images at HathiTrust)
• Langley Research Center: A hybrid computer program for rapidly solving flowing or static chemical kinetic problems involving many chemical species (U.S. National Aeronautics and Space Administration ;, 1976), also by Allen G. McLain, C. S. R. Rao, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Hybrid routing technique for a fault-tolerant, integrated information network (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Barry D. Meredith (page images at HathiTrust)
• Langley Research Center: Hybrid state vector methods for structural dynamic and aeroelastic boundary value problems (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Larry Lee Lehman, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Stanford University. Dept. of Aeronautics and Astronautics (page images at HathiTrust)
• Langley Research Center: A hybridized method for computing high-reynolds-number hypersonic flow about blunt bodies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by K. James Weilmuenster, H. Harris Hamilton, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Hydrodynamic aspects of shark scales (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986), also by William Raschi, John A. Musick, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The hydrodynamic characteristics of a submerged lifting surface having a shape suitable for hydro-ski application (National Aeronautics and Space Administration, 1959), also by Victor L. Vaughan (page images at HathiTrust)
• Langley Research Center: Hydroelastic vibration analysis of partially liquid-filled shells using a series representation of the liquid (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Jerrold M. Housner, John L. Sewall, Robert W. Herr, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Hyperbolic/parabolic development for the GIM-STAR code (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by L. W. Spradley, A. W. Ratliff, J. F. Stalnaker, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Hypersonic aerodynamic characteristics of a family of power-law, wing-body configuratioons (National Aeronautics and Space Administration ;, 1973), also by James C. Townsend (page images at HathiTrust)
• Langley Research Center: Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles (National Aeronautics and Space Administration ;, 1972), also by James P. Arrington and William C. Woods (page images at HathiTrust)
• Langley Research Center: Hypersonic airframe structures technology needs and flight test requirements (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by J. E. Stone, McDonnell Douglas Corporation, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and L. C. Koch (page images at HathiTrust)
• Langley Research Center: Hypersonic cruise vehicle wing structure evaluation (National Aeronautics and Space Administration, 1970), also by Kenneth A. Mason, P. P. Plank, United States National Aeronautics and Space Administration, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Langley Research Center: Hyperthermia as an antineoplastic treatment modality : proceedings of a symposium (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Anas M. El-Mahdi, James Shaeffer, Sheila Ann T. Long, and Eastern Virginia Medical School (page images at HathiTrust)
• Langley Research Center: HZETRN : a heavy ion/nucleon transport code for space radiations (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by John W. Wilson (page images at HathiTrust)
• Langley Research Center: Ideal-gas tables for helium flow in the Mach number range from 40 to 100 (National Aeronautics and Space Administration, 1962), also by James N. Mueller (page images at HathiTrust)
• Langley Research Center: Identification of linear systems by an asymptotically stable observer (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Minh Q. Phan (page images at HathiTrust)
• Langley Research Center: Identification of visual evoked response parameters sensitive to pilot mental state (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by G. L. Zacharias (page images at HathiTrust)
• Langley Research Center: Ignition of mixtures of SiH₄, CH₄, O₂, and Ar or N₂ behind reflected shock waves (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Allen G. McLain, R. Clayton Rogers, and Casimir J. Jachimowski (page images at HathiTrust)
• Langley Research Center: An image compression survey and alogorithm switching based on scene activity (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Michael M. Hart (page images at HathiTrust)
• Langley Research Center: Impact data from a transport aircraft during a controlled impact demonstration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Edwin L. Fasanella, Robert J. Hayduk, and Emilio Alfaro-Bou (page images at HathiTrust)
• Langley Research Center: Impact dynamics research facility for full-scale aircraft crash testing (U.S. National Aeronautics snd Space Administration ;, 1976), also by Victor L. Vaughan and Emilio Alfaro-Bou (page images at HathiTrust)
• Langley Research Center: The impact of science on society (Scientific and Technical Information Branch, National Aeronautics and Space Administration, 1985), also by James Burke, Isaac Asimov, Jules Bergman, College of William and Mary, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Impact studies of a 1/3-scale model of an air cushion vehicle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Robert H. Daugherty (page images at HathiTrust)
• Langley Research Center: Impact tests on fibrous composite sandwich structures (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Marvin D. Rhodes and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Impacts of technology on the capacity needs of the U.S. national airspace systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Raymond A. Ausrotas, Robert W. Simpson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: An impedance technique for determining low-frequency payload environments (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Kenneth R. Payne and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Imperfection sensitivity of optimum structural designs for a Mars entry capsule (National Aeronautics and Space Administration ;, 1971), also by Gerald A. Cohen and Philco-Ford Corporation (page images at HathiTrust)
• Langley Research Center: Implications of outer-zone radiations on operations in the geostationary region utilizing the AE4 environmental model (National Aeronautics and Space Administration ;, 1977), also by John W. Wilson, Fred M. Denn, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An implicit characteristic based method for electromagnetics (National Aeronautics and Space Administration, Langley Research Center, 2001), also by John H. Beggs and W. Roger Briley (page images at HathiTrust)
• Langley Research Center: An implicit finite-difference solution to the viscous shock layer, including the effects of radiation and strong blowing (National Aeronautics and Space Administration ;, 1972), also by L. Bernard Garrett, John N. Perkins, and G. Louis Smith (page images at HathiTrust)
• Langley Research Center: An implicit method for the calculation of inlet flow fields (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Sedat Biringen, Oden J. McMillan, Nielsen Engineering & Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Importance of the variation of drag with lift in minimization of satellite entry acceleration (National Aeronautics and Space Administration, 1959), also by Frederick C. Grant (page images at HathiTrust)
• Langley Research Center: Improved analysis of electron penetration and numerical procedures for space radiation shielding (National Aeronautics and Space Administration ;, 1977), also by John W. Wilson, Fred M. Denn, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An improved analytical treatment of the denting of thin sheets by hail (National Aeronautics and Space Administration, 1971), also by Robert G. Thomson, Robert J. Hayduk, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An improved computational procedure for determining helicopter rotor blade natural modes (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by William H. Weller, Raymond E. Mineck, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Improved empirical model for base drag prediction on missile configurations based on new wind tunnel data (Dahlgren, Virginia : Weapons Systems Department, Naval Surface Warfare Center, Dahlgren Division, 1992., 1992), also by Frank G. Moore, Floyd J. Wilcox, Tom Hymer, and Naval Surface Warfare Center (U.S.). Dahlgren Division (page images at HathiTrust)
• Langley Research Center: Improved equivalent linearization implementations using nonlinear stiffness evaluation (National Aeronautics and Space Administration, Langley Research Center, 2001), also by Stephen A. Rizzi and Alexander A. Muravyov (page images at HathiTrust)
• Langley Research Center: An improved exceedance theory for combined random stresses (National Aeronautics and Space Administration ;, 1974), also by Harold C. Lester (page images at HathiTrust)
• Langley Research Center: Improved guidance hardware study for the Scout launch vehicle (National Aeronautics and Space Administration ;, 1972), also by Roger T. Schappel and Martin Marietta Corporation (page images at HathiTrust)
• Langley Research Center: An improved lambda-scheme for one-dimensional flows (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Gino Moretti, Michael T. DiPiano, Inc G.M.A.F., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Improved low-cost inorganic organic separators for rechargeable silver-zinc batteries (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Dean W. Sheibley and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: An improved method for calculating supersonic pressure fields about bodies of revolution (National Aeronautics and Space Administration, 1971), also by Robert J. Mack and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An improved method for design of expansion-chamber mufflers with application to an operational helicopter (National Aeronautics and Space Administration ;, 1973), also by Tony L. Parrott and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An improved method for optimum design of mechanically and thermally loaded structures (National Aeronautics and Space Administration ;, 1975), also by Howard M. Adelman, R. Narayanaswami, and Joanne L. Walsh (page images at HathiTrust)
• Langley Research Center: An improved method for the aerodynamic analysis of wing-body-tail configurations in subsonic and supersonic flow (National Aeronautics and Space Administration ;, 1973), also by F. A. Woodward and Aerophysics Research Corporation (page images at HathiTrust)
• Langley Research Center: Improved model for solar cosmic ray exposure in manned earth orbital flights (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by John W. Wilson (page images at HathiTrust)
• Langley Research Center: Improved simulation of aerosol, cloud, and density measurements by shuttle lidar (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Philip B. Russell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An improved supersonic, three-dimensional, external, inviscid flow field code (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Frank Marconi, Frank Koch, Grumman Aerospace Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Improved tangent-cone method for the Aerodynamic Preliminary Analysis System (APAS) version of the Hypersonic Arbitrary-Body Program (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Christopher I. Cruz and Gregory J. Sova (page images at HathiTrust)
• Langley Research Center: An improved transverse shear deformation theory for laminated anisotropic plates (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by M. V. V. Murthy and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An improved version of NCOREL : a computer program for 3-D nonlinear supersonic potential flow computations (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Michael J. Siclari (page images at HathiTrust)
• Langley Research Center: An improved Woodward's panel method for calculating leading-edge and side-edge suction forces at subsonic and supersonic speed (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by C. Edward Lan, Sudhir C. Mehrotra, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Improvement in the quality of flow visualization in the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by W. L. Snow, William K. Goad, and Alpheus W. Burner (page images at HathiTrust)
• Langley Research Center: Improvements in computational accuracy of BRYNTRN (a baryon transport code) (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Judy L. Shinn (page images at HathiTrust)
• Langley Research Center: Improvements to the FATOLA computer program including nosewheel steering : supplemental instruction manual (National Aeronautics and Space Administration, Scientific and Technical Information ;, 1978), also by Huey D. Carden, John R. McGehee, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Improvements to the missile aerodynamic prediction code DEMON3 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Marnix F. E. Dillenius, Daniel J. Lesieutre, David L. Johnson, and Inc Nielsen Engineering & Research (page images at HathiTrust)
• Langley Research Center: An in-flight simulation of lateral control nonlinearities (National Aeronautics and Space Administration ;, 1975), also by David R. Ellis, Narayan W. Tilak, and Princeton University. Flight Research Laboratory (page images at HathiTrust)
• Langley Research Center: In situ sensors for measurements in the global troposphere (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by M. L. Saeger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Incipient- and developed-spin and recovery characteristics of a modern high-speed fighter design with low aspect ratio as determined from dynamic-model tests (National Aeronautics and Space Administration, 1961), also by Henry A. Lee, Charles E. Libbey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Inclusive inelastic scattering of heavy ions and nuclear correlations (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Francis A. Cucinotta (page images at HathiTrust)
• Langley Research Center: Incorporation of coupled nonequilibrium chemistry into a two-dimensional nozzle code (SEAGULL) (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by A. W. Ratliff, Lockheed Missiles and Space Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Induced drag ideal efficiency factor of arbitrary lateral-vertical wing forms (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by John DeYoung and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Induced interference effects on the aerodynamic characteristics of a 0.16-scale six-jet V / by Matthew M. Winston. (National Aeronautics and Space Administration :, 1970), also by Matthew M. Winston and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Induced pressure distribution of a jet in a crossflow (National Aeronautics and Space Administration ;, 1975), also by Richard L. Fearn and Robert P. Weston (page images at HathiTrust)
• Langley Research Center: Industry workshop on large space structures, executive summary (U.S. National Aeronautics and Space Administration ;, 1976), also by Ellis Katz, United States National Aeronautics and Space Administration, and McDonnell Douglas Astronautics Company (page images at HathiTrust)
• Langley Research Center: An inexpensive economical solar heating system for homes (U.S. National Aeronautics and Space Administration ;, 1976), also by Johnny W. Allred and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Inflation and performance of three parachute configurations from supersonic flight tests in a low-density environment (NASA, 1969), also by Charles H. Whitlock, Richard J. Bendura, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Richard M. Wood, Gary F. Wesselmann, and James E. Byrd (page images at HathiTrust)
• Langley Research Center: Influence of configuration details on the subsonic characteristics of a space shuttle orbiter design (National Aeronautics and Space Administration ;, 1974), also by John P. Decker and W. Pelham Phillips (page images at HathiTrust)
• Langley Research Center: Influence of display and control compatibility on pilot-induced oscillations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Marvin C. Waller, Lee H. Person, Randall L. Harris, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: The influence of low wall temperature on boundary-layer transition and local heat transfer on 2-inch-diameter hemispheres at a Mach number of 4.95 and a Reynolds number per foot of 73.2 x 10⁶ (National Aeronautics and Space Administration, 1960), also by Morton Cooper, Jerome D. Julius, and Edward E. Mayo (page images at HathiTrust)
• Langley Research Center: Influence of nonequilibrium radiation and shape change on aerothermal environment of a Jovian entry body (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by S. N. Tiwari, S. V. Subramanian, Old Dominion University. Research Foundation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Influence of orbital-maneuvering-system fairings and rudder flare on the transonic aerodynamic characteristics of a space shuttle orbiter (National Aeronautics and Space Administration ;, 1975), also by James C. Ellison (page images at HathiTrust)
• Langley Research Center: Influence of particle drag coefficient on particle motion in high-speed flow with typical laser velocimeter applications (National Aeronautics and Space Administration ;, 1976), also by Michael J. Walsh (page images at HathiTrust)
• Langley Research Center: Influence of programing techniques and of varying limit load factors on maneuver load fatigue test results (National Aeronautics and Space Administration, 1966), also by Patrick L. Corbin, Eugene C. Naumann, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Influence of salt and elevated-temperature exposure on the maximum compressive strength of titanium-alloy skin-stringer panels (National Aeronautics and Space Administration ;, 1970), also by James E. Gardner and Dick M. Royster (page images at HathiTrust)
• Langley Research Center: Influence of solar radiation pressure on orbital eccentricity of a gravity-gradient-oriented lenticular satellite (National Aeronautics and Space Administration, 1965), also by William M. Adams, Ward F. Hodge, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Influence of surface static-pressure orifices on boundary-layer transition (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1982), also by Dan M. Somers and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Influence of upstream flow discontinuities on the acoustic power radiated by a model air jet (National Aeronautics and Space Administration ;, 1967), also by Colin G. Gordon, Gideon Maidanik, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Influence of utility lines and thermal blankets on the dynamics and control of satellites with precision pointing requirements (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Richard K. Miller, John M. Hedgepeth, Mark W. Thomson, Astro Aerospace Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Langley Research Center: Influence of various fabrication methods on the compressive strength of titanium skin-stringer panels (National Aeronautics and Space Administration ;, 1969), also by Richard A. Pride, James E. Gardner, Dick M. Royster, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The Influence of wing loading on turbofan powered STOL transports with and without externally blown flaps (National Aeronautics and Space Administration ;, 1973), also by R. L. Morris and Boeing Company. Wichita Division (page images at HathiTrust)
• Langley Research Center: Information and display requirements for independent landing monitors (National Aeronautics and Space Administration ;, 1976), also by J. S. Karmarkar, J. A. Sorenson, United States National Aeronautics and Space Administration, and inc Systems Control (page images at HathiTrust)
• Langley Research Center: Infrared measurements of a scramjet exhaust (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by R. A. Reed and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: InGaAsP/InP laser development for single-mode, high-data-rate communications (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by I. Ladany, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and RCA Laboratories (page images at HathiTrust)
• Langley Research Center: Initial conceptual design study of self-critical nuclear pumped laser systems (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Richard J. Rodgers and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Initiation precursors and initiators in laser-induced copolymerization of styrene and maleic anhydride in acetone (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Gilda A. Miner, C. Ken Chang, and Willard E. Meador (page images at HathiTrust)
• Langley Research Center: Injection efficiency of bound modes (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Claudio Oliveira Egalon, College of William and Mary. Dept. of Physics, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Langley Research Center: An Inlet analysis for the NASA hypersonic research engine aerothermodynamic integration model (National Aeronautics and Space Administration ;, 1974), also by Earl H. Andrews (page images at HathiTrust)
• Langley Research Center: Input admittance of a rectangular waveguide-fed aperture antenna radiating into an inhomogeneous lossy dielectric slab (National Aeronautics and Space Administration ;, 1967), also by Calvin T. Swift (page images at HathiTrust)
• Langley Research Center: InSb charge coupled infrared imaging device--20-element linear imager (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by R. D. Thom and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Edwin E. Lee and Odis C. Pendergraft (page images at HathiTrust)
• Langley Research Center: Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17 scale, twin-engine, low-wing transport model (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Odis C. Pendergraft (page images at HathiTrust)
• Langley Research Center: Instrument error analysis as it applies to wind-tunnel testing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Emanuel Rind and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Instrument scanning and controlling : using eye movement data to understand pilot behavior and strategies (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), also by A. O. Dick (page images at HathiTrust)
• Langley Research Center: Instrumentation of sampling aircraft for measurement of launch vehicle effluents (National Aeronautics and Space Administration ;, 1977), also by Dewey E. Wornom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An integral equation formulation for predicting radiation patterns of a space shuttle annular slot antenna (National Aeronautics and Space Administration ;, 1974), also by J. Earl Jones and J. H. Richmond (page images at HathiTrust)
• Langley Research Center: An integral-equation solution for TE radiation and scattering from conducting cylinders (National Aeronautics and Space Administration ;, 1973), also by J. H. Richmond and Ohio State University (page images at HathiTrust)
• Langley Research Center: Integrated active and passive control design methodology for the LaRC CSI evolutionary model (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Christopher T. Voth (page images at HathiTrust)
• Langley Research Center: Integrated airframe propulsion control (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Robert E. Fennell, Stephen B. Black, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Integrated application of active controls (IACC) technology to an advanced subsonic transport : project plan (National Aeronautics and Space Admininstration, Scientific and Technical Information Branch ;, 1981), also by Boeing Commercial Airplane Company and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Integrated autopilot/autothrottle based on a total energy control concept : design and evaluation of additional autopilot modes (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Kevin R. Bruce (page images at HathiTrust)
• Langley Research Center: Integrated autopilot/autothrottle for the NASA TSRV B-737 aircraft : design and verification by nonlinear simulation (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1989), also by Kevin R. Bruce (page images at HathiTrust)
• Langley Research Center: An integrated computer procedure for sizing composite airframe structures (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Jaroslaw Sobieszczanski-Sobieski and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Integrated Power/Attitude Control System (IPACS) study (National Aeronautics and Space Administration ;, 1974), also by J. E. Notti and Rockwell International. Space Division (page images at HathiTrust)
• Langley Research Center: Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Milton Lamb and William Kelly Abeyounis (page images at HathiTrust)
• Langley Research Center: Interaction between a normal shock wave and a turbulent boundary layer at high, transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Thomas Charles Adamson, Arthur F. Messiter, M. S. Liou, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Interaction between step fuel injectors on opposite walls in a supersonic combustor model (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Charles R. McClinton and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Interaction of the space shuttle control system with pogo (National Aeronautics and Space Administration ;, 1972), also by A. Stewart Hopkins, William F. Davis, and McDonnell Douglas Astronautics Company-Huntington Beach (page images at HathiTrust)
• Langley Research Center: Interactions of Tollmien-Schlichting waves and Dean vortices : comparison of direct numerical simulation and a weakly nonlinear theory (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Bart A. Singer and Thomas A. Zang (page images at HathiTrust)
• Langley Research Center: Interactive design and analysis of future large spacecraft concepts (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by L. Bernard Garrett and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An interactive user-friendly approach to surface-fitting three-dimensional geometries (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by F. McNeil Cheatwood and Fred R. DeJarnette (page images at HathiTrust)
• Langley Research Center: Interference between exhaust system and afterbody of twin-engine fuselage configurations (National Aeronautics and Space Administration ;, 1974), also by Jack F. Runckel (page images at HathiTrust)
• Langley Research Center: Interference drag in a simulated wing-fuselage juncture (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by L. Kubendran, J. Hubbartt, H. McMahon, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Interference heating from interactions of shock waves with turbulent boundary layers at Mach 6 (National Aeronautics and Space Administration ;, 1974), also by Charles B. Johnson and Louis G. Kaufman (page images at HathiTrust)
• Langley Research Center: Interference heating on a swept cylinder in region of intersection with a wedge at Mach number 8 (National Aeronautics and Space Administration ;, 1965), also by Dennis M. Bushnell (page images at HathiTrust)
• Langley Research Center: Interference of oxygen, carbon dioxide, and water vapor on the analysis for oxides of nitrogen by chemiluminescence (National Aeronautics and Space Administration ;, 1975), also by Howard G. Maahs (page images at HathiTrust)
• Langley Research Center: The interlaminar fracture toughness of woven graphite/epoxy composites (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Joan G. Funk and Jerry W. Deaton (page images at HathiTrust)
• Langley Research Center: Intermediate energy proton-deuteron elastic scattering (National Aeronautics and Space Administration ;, 1973), also by John W. Wilson (page images at HathiTrust)
• Langley Research Center: Internal convective cooling systems for hypersonic aircraft (National Aeronautics and Space Administration ;, 1975), also by Frank M. Anthony, Robert G. Helenbrook, W. H. Dukes, and Bell Aerospace Textron (page images at HathiTrust)
• Langley Research Center: Internal performance of a hybrid axisymmetric/nonaxisymmetric convergent-divergent nozzle (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by John G. Taylor (page images at HathiTrust)
• Langley Research Center: Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Bobby L. Berrier and John G. Taylor (page images at HathiTrust)
• Langley Research Center: International Symposium on Magnetic Suspension Technology : proceedings of an international symposium sponsored by the National Aeronautics and Space Administration, Washington, D.C., and held at Langley Research Center, Hampton, Virginia, August 19-23, 1991 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program , 1992), also by International Symposium on Magnetic Suspension Technology (1991 : Langley Research Center), Colin P. Britcher, Nelson J. Groom, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Interpretation methodology and analysis of in-flight lightning data (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Terence Rudolph, Rodney A. Perala, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Research Triangle Institute, and Inc Electro Magnetic Applications (page images at HathiTrust)
• Langley Research Center: The interpretation of nonlinear pitching moments in relation to the pitch-up problem (National Aeronautics and Space Administration, 1959), also by George S. Campbell and Joseph Weil (page images at HathiTrust)
• Langley Research Center: Interpreter composition issues in the formal verification of a processor-memory module (National Aeronautics and Space Administration, Langley Research Center ;, 1994), also by David A. Fura and Gerald C. Cohen (page images at HathiTrust)
• Langley Research Center: Intersection of three-dimensional geometric surfaces (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Vicki K. Crisp, James L. Schwing, and John J. Rehder (page images at HathiTrust)
• Langley Research Center: Inverse boundary-layer theory and comparsion with experiment (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by James E. Carter and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Inverse solutions for laminar boundary-layer flows with separation and reattachment (National Aeronautics and Space Administration ;, 1975), also by James E. Carter (page images at HathiTrust)
• Langley Research Center: An investigation at subsonic speeds of aerodynamic charactersitcs at angles of attack from -4⁰ to 100⁰ of a delta-wing reentry configuration having folding wingtip panels (National Aeronautics and Space Administration, Langley Research Center, 1960), also by Bernard Spencer (page images at HathiTrust)
• Langley Research Center: Investigation at transonic speeds to determine lateral control effectiveness of blowing laterally over surfaces of 30° and 45° swept wings (National Aeronautics and Space Administration, 1959), also by Alexander D. Hammond and Linwood W. McKinney (page images at HathiTrust)
• Langley Research Center: Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds (National Aeronautics and Space Administration, 1960), also by Mary W. Jackson and K. R. Czarnecki (page images at HathiTrust)
• Langley Research Center: Investigation, development and application of optimal output feedback theory. Volume IV, Measures of eigenvalue/eigenvector sensitivity to system parameters and unmodeled dynamics (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by Nesim Halyo and inc Information & Control Systems (page images at HathiTrust)
• Langley Research Center: An investigation for the development of an integrated optical data preprocesssor (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by C. M. Verber and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Investigation of a 4.0-inch-mean-diameter four-stage reentry turbine for auxiliary power drives (National Aeronautics and Space Administration, 1960), also by Robert Y. Wong, Monroe Daniel E., David L. Darmstadt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An investigation of a close-coupled canard as a direct side-force generator on a fighter model at Mach numbers from 0.40 to 0.90 (National Aeronautics and Space Administration ;, 1977), also by Richard J. Re, Francis J. Capone, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Investigation of a jet condenser for space power (National Aeronautics and Space Administration ;, 1965), also by Robert J. Platt (page images at HathiTrust)
• Langley Research Center: Investigation of a plasma accelerator with magnetic field arranged to produce a divergent-nozzle effect (National Aeronautics and Space Administration ;, 1969), also by Joseph D. Brooks and William D. Beasley (page images at HathiTrust)
• Langley Research Center: An investigation of a sterile access technique for the repair and adjustment of sterile spacecraft (National Aeronautics and Space Administration ;, 1973), also by Franklin H. Farmer, Richard M. Hueschen, and Harry V. Fuller (page images at HathiTrust)
• Langley Research Center: Investigation of a supersonic cruise fighter model flow field (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by David E. Reubush and E. Ann Bare (page images at HathiTrust)
• Langley Research Center: Investigation of an anomalous flow condition of the Langley pilot model expansion tube (National Aeronautics and Space Administration ;, 1974), also by Wilfred J. Friesen (page images at HathiTrust)
• Langley Research Center: Investigation of an automatic spin-prevention system for fighter airplanes (National Aeronautics and Space Administration, 1972), also by William P. Gilbert, Charles E. Libbey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Investigation of an optimum detection scheme for a star-field mapping system (National Aeronautics and Space Administration, 1970), also by Melvin D. Aldridge, Leonard Credeur, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Investigation of atomic oxygen-surface interactions related to measurements with dual air density explorer satellites (National Aeronautics and Space Administration ;, 1973), also by B. J. Wood, Henry Wise, C. M. Ablow, and Stanford Research Institute (page images at HathiTrust)
• Langley Research Center: Investigation of Axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Francis J. Capone, Bobby L. Berrier, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Investigation of blown boundary layers with an improved wall jet system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by K. R. Saripalli, R. L. Simpson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Investigation of bremsstrahlung production in spacecraft materials (National Aeronautics and Space Administration ;, 1969), also by W. E. Dance, W. J. Rainwater, and Ling-Temco-Vought (page images at HathiTrust)
• Langley Research Center: Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Bobby L. Berrier, Richard J. Re, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: An investigation of correlation between pilot scanning behavior and workload using stepwise regression analysis (U.S. National Aeronautics and Space Administration ;, 1976), also by Marvin C. Waller and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Investigation of DC-8 nacelle modifications to reduce fan-compressor noise in airport communities (National Aeronautics and Space Administration ;, 1970), also by Douglas Aircraft Company (page images at HathiTrust)
• Langley Research Center: Investigation of degradation mechanisms on complete matrices (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1982), also by C. Giori, T. Yamauchi, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and IIT Research Institute (page images at HathiTrust)
• Langley Research Center: Investigation of double slotted flaps on a swept-wing transport model (National Aeronautics and Space Administration, 1959), also by Rodger L. Naeseth and Edwin E. Davenport (page images at HathiTrust)
• Langley Research Center: Investigation of effect of propulsion system installation and operation on aerodynamics of an airbreathing hypersonic airplane at Mach O.3 to 1.2 (National Aeronautics and Space Administration ;, 1977), also by James M. Cubbage, Charles E. Mercer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Investigation of effects of microphone position and orientation on near-ground noise measurements (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by William L. Willshire, Paul A. Nystrom, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Investigation of electron-radiation-induced dielectric breakdowns in a typical capacitor meteoroid detector system (National Aeronautics and Space Administration ;, 1968), also by George M. Storti and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Investigation of flow-field development for a series of sonic-boom wind-tunnel models (National Aeronautics and Space Administration ;, 1971), also by Harry L. Runyan and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An investigation of fracture toughness, fatigue-crack growth, sustained-load flaw growth, and impact properties of three pressure vessel steels (National Aeronautics and Space Administration ;, 1975), also by Charles Michael Hudson, Peter E. Lewis, and J. C. Newman (page images at HathiTrust)
• Langley Research Center: An investigation of heat transfer within regions of separated flow at a Mach number of 6.0 (National Aeronautics and Space Administration ;, 1965), also by Paul F. Holloway, Helen S. Creekmore, and James R. Sterrett (page images at HathiTrust)
• Langley Research Center: Investigation of high temperature antennas for space shuttle (National Aeronautics and Space Administration ;, 1973), also by E. A. Kuhlman and McDonnell Douglas Astronautics Company-East (page images at HathiTrust)
• Langley Research Center: An investigation of high-velocity impact cratering into nonmetallic targets and correlation of penetration data for metallic and nonmetallic targets (National Aeronautics and Space Administration, 1961), also by William H. Kinard and Rufus Davis Collins (page images at HathiTrust)
• Langley Research Center: Investigation of lateral-directional dynamic stability of a tilt-wing V/STOL transport (National Aeronautics and Space Administration :, 1970), also by Joseph R. Chambers, Sue B. Grafton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Peter F. Covell, David S. Miller, and Richard M. Wood (page images at HathiTrust)
• Langley Research Center: An investigation of leakage of large-diameter O-ring seals on spacecraft air-lock hatches (National Aeronautics and Space Administration ;, 1968), also by Otto F. Trout (page images at HathiTrust)
• Langley Research Center: Investigation of light scattering as a technique for detecting discrete soot particles in a luminous flame (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by David R. Schryer and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Investigation of microstructural changes in polyetherether-ketone films at cryogenic temperatures by positron lifetime spectroscopy (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Jag J. Singh (page images at HathiTrust)
• Langley Research Center: An Investigation of microstructural characteristics of contact-lens polymers (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Jag J. Singh (page images at HathiTrust)
• Langley Research Center: Investigation of net-thrust and base-pressure characteristics of cylindrical afterbodies with clustered supersonic nozzles at transonic Mach numbers (National Aeronautics and Space Administration, 1961), also by Earl H. Andrews and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An investigation of new methods for estimating parameter sensitivities (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Todd J. Beltracchi, Gary A. Gabriele, and Rensselaer Polytechnic Institute (page images at HathiTrust)
• Langley Research Center: Investigation of new radar-data-reduction techniques used to determine drag characteristics of a free-flight vehicle (National Aeronautics and Space Administration ;, 1974), also by Gerard E. Woodbury and John W. Wallace (page images at HathiTrust)
• Langley Research Center: Investigation of nonlinear inviscid and viscous flow effects in the analysis of dynamic stall (National Aeronautics and Space Administration ;, 1974), also by Peter Crimi and Avco Corporation. Systems Division (page images at HathiTrust)
• Langley Research Center: An investigation of nonpropagating fatigue cracks (National Aeronautics and Space Administration, 1959), also by A. J. McEvily and Walter Illg (page images at HathiTrust)
• Langley Research Center: Investigation of occultation and imagery problems for orbital missions to Venus and Mars (National Aeronautics and Space Administration ;, 1969), also by Richard N. Green (page images at HathiTrust)
• Langley Research Center: Investigation of phase-change coatings for variable thermal control of spacecraft (National Aeronautics and Space Administration ;, 1972), also by Warren C. Kelliher and Philip R. Young (page images at HathiTrust)
• Langley Research Center: An investigation of photosensor aperture shaping in facsimile cameras (National Aeronautics and Space Administration ;, 1972), also by S. J. Katzberg, Stephen D. Wall, and Friedrich O. Huck (page images at HathiTrust)
• Langley Research Center: Investigation of problems associated with the use of alloyed molybdenum sheet in structures at elevated temperatures (National Aeronautics and Space Administration :, 1960), also by Eldon E. Mathauser, Donald R. Rummler, and Bland A. Stein (page images at HathiTrust)
• Langley Research Center: Investigation of ramp injectors for supersonic mixing enhancement (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Y. Haimovitch, A. S. Roberts, and E. Gartenberg (page images at HathiTrust)
• Langley Research Center: Investigation of responsivity and noise in a direct-coupled photodetector-preamplifier for facsimile cameras (National Aeronautics and Space Administration ;, 1973), also by W. Lane Kelly, S. J. Katzberg, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An investigation of several NACA 1-series axisymmetric inlets at Mach numbers from 0.4 to 1.29 (National Aeronautics and Space Administration ;, 1974), also by Richard J. Re (page images at HathiTrust)
• Langley Research Center: An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0 (U.S. National Aeronautics and Space Administration ;, 1976), also by Richard J. Re (page images at HathiTrust)
• Langley Research Center: An investigation of size-dependent concentration of trace elements in aerosols emitted from the oil-fired heating plants (U.S. National Aeronautics and Space Administration ;, 1976), also by Jag J. Singh, G. S. Khandelwal, R. J. Sentell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Investigation of some effects of flexibility on the lift and pitching-moment characteristics of a series of low-aspect- ratio wing-body combinations at transonic speeds (National Aeronautics and Space Administration, 1960), also by Robert V. Doggett and A. Gerald Rainey (page images at HathiTrust)
• Langley Research Center: Investigation of tethered station keeping (National Aeronautics and Space Administration ;, 1967), also by James R. Williams and James J. Adams (page images at HathiTrust)
• Langley Research Center: Investigation of the aerodynamic characteristics of a 0.067-scale model of the x-15 airplane (configuration 3) at mach numbers of 2.29, 2.98, and 4.65 (National Aeronautics and Space Administration, 1959), also by Arthur E. Franklin and Robert M. Lust (page images at HathiTrust)
• Langley Research Center: Investigation of the aerodynamic characteristics of a hypersonic transport model at Mach numbers to 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1971), also by James C. Ellison and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Investigation of the aerodynamic characteristics of a supersonic horizontal- attitude VTOL airplane model at Mach numbers of 1.57, 2.14, 2.54, and 2.87 (National Aeronautics and Space Administration, 1960), also by Arthur E. Franklin and Robert M. Lust (page images at HathiTrust)
• Langley Research Center: Investigation of the aerodynamic characteristics of two preliminary designs of Scout research vehicle at Mach numbers from 1.77 to 4.65 (National Aeronautics and Space Administration, 1961), also by Robert J. Keynton and Ann B. Fichter (page images at HathiTrust)
• Langley Research Center: Investigation of the applicability of the free-wing principle to light, general aviation aircraft (National Aeronautics and Space Administration ;, 1972), also by Richard F. Porter, Joe H. Brown, Ross G. Luce, and Battelle Memorial Institute. Columbus Laboratories (page images at HathiTrust)
• Langley Research Center: Investigation of the effect of a guide-vane-rotor combination on inlet total-pressure distortions in a compressible fluid (National Aeronautics and Space Administration, 1959), also by George C. Ashby (page images at HathiTrust)
• Langley Research Center: Investigation of the effect of downwash from a vertical takeoff and landing aircraft and a helicopter in the ground environment (National Aeronautical and Space Administration, 1961), also by Thomas C. O'Bryan and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An investigation of the effect of high temperature on the Schumann-Runge ultraviolet absorption continuum of oxygen (National Aeronautics and Space Administration :, 1961), also by John S. Evans and Charles J. Schexnayder (page images at HathiTrust)
• Langley Research Center: Investigation of the effects of cobalt ions on epoxy properties (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Jag J. Singh and Diane M. Stoakley (page images at HathiTrust)
• Langley Research Center: Investigation of the effects of inlet shapes on fan noise radiation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by T. L. Clark, P. G. Vaidya, D. R. Slotboom, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Investigation of the effects of long duration space exposure on active optical system components (National Aeronautics and Space Administration, Langley Research Center, 1994), also by M. D. Blue (page images at HathiTrust)
• Langley Research Center: Investigation of the effects of nonhomogeneous (or nonstationary) behavior on the spectra of atmospheric turbulence (U.S. National Aeronautics and Space Administration ;, 1976), also by William D. Mark, Raymond W. Fischer, and Beranek Bolt (page images at HathiTrust)
• Langley Research Center: An investigation of the effects of surrounding structure on sonic fatigue (National Aeronautics and Space Administration, 1970), also by Thomas F. Nelson, United States National Aeronautics and Space Administration, and Lockheed-Georgia Company (page images at HathiTrust)
• Langley Research Center: An investigation of the facsimile camera response to object motion (National Aeronautics and Space Administration ;, 1974), also by Friedrich O. Huck, Ernest E. Burcher, and Stephen D. Wall (page images at HathiTrust)
• Langley Research Center: An investigation of the fine-pointing control system of a soft-gimbaled orbiting telescope (National Aeronautics and Space Administration, 1970), also by Frederick R. Morrell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Investigation of the flow over a spiked-nose hemisphere-cylinder at a Mach number of 6.8 (National Aeronautics and Space Administration, 1959), also by Davis H. Crawford (page images at HathiTrust)
• Langley Research Center: Investigation of the flow over simple bodies at Mach numbers of the order of 20 (National Aeronautics and Space Administration :, 1960), also by Arthur Henderson (page images at HathiTrust)
• Langley Research Center: Investigation of the free-flight characteristics and handling qualities of a ground-effect machine (National Aeronautics and Space Administration, 1967), also by Arthur W. Carter and Lee H. Person (page images at HathiTrust)
• Langley Research Center: Investigation of the growth of garnet films by liquid phase epitaxy (National Aeronautics and Space Administration ;, 1974), also by Jerry W. Moody, Robert M. Sandfort, Roger W. Shaw, and Monsanto Research Corporation (page images at HathiTrust)
• Langley Research Center: An investigation of the high speed turbulent boundary layer with heat transfer and arbitrary pressure gradient (National Aeronautics and Space Administration ;, 1970), also by Constantino Economos, J. L. Boccio, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Langley Research Center: Investigation of the influence of duct-mounted Helmholtz resonators on the sound field of a model ducted propeller (National Aeronautics and Space Administration ;, 1970), also by David Brown and Bell Aerospace Company (page images at HathiTrust)
• Langley Research Center: Investigation of the loading characteristics of the lifting surfaces and the speed brakes of a 0.067-scale model of the north american x-15 airplane (configuration 3) at Mach numbers of 2.29, 2.98, and 4.65 (National Aeronautics and Space Administration, 1960), also by Norman H. Silvers, Jane S. Wills, and Julia A. Lancaster (page images at HathiTrust)
• Langley Research Center: Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration (National Aeronautics and Space Administration, 1962), also by George M. Ware (page images at HathiTrust)
• Langley Research Center: Investigation of the multiple model adaptive control (MMAC) method for flight control systems (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Michael Athans (page images at HathiTrust)
• Langley Research Center: Investigation of the performance characteristics of Doppler radar technique for aircraft collision hazard warning. Phase III. (National Aeronautics and Space Administration ;, 1972), also by Research Triangle Institute (page images at HathiTrust)
• Langley Research Center: An investigation of the role of gaseous diffusion in the oxidation of a metal forming a volatile oxide (National Aeronautics and Space Administration, 1960), also by Jerry L. Modisette and David R. Schryer (page images at HathiTrust)
• Langley Research Center: Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode (National Aeronautics and Space Administration ;, 1974), also by Jarrett K. Huffman and Charlie M. Jackson (page images at HathiTrust)
• Langley Research Center: Investigation of the static longitudinal and lateral stability characteristics of a 0.10-scale model of a three-stage configuration of the Scout research vehicle at Mach numbers of 2.29, 2.96, 3.96, and 4.65 (National Aeronautics and Space Administration, 1961), also by Lloyd S. Jernell (page images at HathiTrust)
• Langley Research Center: Investigation of the static longitudinal stability characteristics of a 0.067-scale model of a four-stage configuration of the Scout research vehicle at Mach numbers of 2.29, 2.96, 3.96, and 4.65 (National Aeronautics and Space Administration, 1960), also by Lloyd S. Jernell and Norman D. Wong (page images at HathiTrust)
• Langley Research Center: Investigation of the static longitudinal stability characteristics of an air-to-surface canard missile configuration in the transonic mach number range (National Aeronautics and Space Administration, 1960), also by Gerald L. Hunt (page images at HathiTrust; US access only)
• Langley Research Center: Investigation of the static stability characteristics of a reentry spacecraft model in free flight for Mach numbers from 2.62 to 1.11 launched at an angle of attack of 180 degree (National Aeronautics and Space Administration, 1961), also by J. W. Usry (page images at HathiTrust)
• Langley Research Center: Investigation of the subsonic and supersonic release characteristics of an externally carried fuel tank from a 1/40-scale model of a bomber airplane (National Aeronautics and Space Administration, 1961), also by William F. Hinson (page images at HathiTrust)
• Langley Research Center: Investigation of the vibration isolation of commercial jet transport pilots during turbulent air penetration (National Aeronautics and Space Administration, 1970), also by Dale W. Schubert, Frank E. Roman, Jerome S. Pepi, United States National Aeronautics and Space Administration, and Barry Wright Corporation (page images at HathiTrust)
• Langley Research Center: An investigation of the visual sampling behaviour of human observers (For sale by the Clearinghouse for Federal Scientific and Technical Information, 1966), also by John W. Senders and Beranek Bolt (page images at HathiTrust)
• Langley Research Center: Investigation of thermal fatigue in fiber composite materials (U.S. National Aeronautics and Space Administration ;, 1976), also by Abdel A. Fahmy, Thomas G. Cunningham, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Investigation of variation in base pressure over the Reynolds number range in which wake transition occurs for two-dimensional bodies at Mach numbers from 1.95 to 2.92 (National Aeronautics and Space Administration, 1959), also by Vernon Van Hise (page images at HathiTrust)
• Langley Research Center: Investigation of vibration characteristics of circular-arc monocoque beams (National Aeronautics and Space Administration, 1959), also by W. B. Fichter and Eldon E. Kordes (page images at HathiTrust)
• Langley Research Center: An investigation to determine conditions under which downwash from VTOL aircraft will start surface erosion from various types of terrain (National Aeronautics and Space Administration, 1959), also by Richard E. Kuhn (page images at HathiTrust)
• Langley Research Center: Investigations of a flow field surrounding circular-arc boattail nozzles at subsonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by William Kelly Abeyounis, Lawrence E. Putnam, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Investigations of high power problems in space shuttle antenna designs (National Aeronautics and Space Administration ;, 1972), also by William C. Taylor, N. J. Alvares, and Stanford Research Institute (page images at HathiTrust)
• Langley Research Center: Ion heating in a plasma focus (National Aeronautics and Space Administration ;, 1974), also by Frank Hohl and S. Peter Gary (page images at HathiTrust)
• Langley Research Center: Ionization and deionization processes in low-density plasma flows (National Aeronautics and Space Administration, 1961), also by Raymond L. Barger (page images at HathiTrust)
• Langley Research Center: Irradiation effects of 22 and 240 Mev protons on several transistors and solar cells (National Aeronautics and Space Administration, 1961), also by William C. Hulten, John L. Patterson, and William C. Honaker (page images at HathiTrust)
• Langley Research Center: Isosinglet approximation for nonelastic reactions (National Aeronautics and Space Administration ;, 1972), also by John W. Wilson (page images at HathiTrust)
• Langley Research Center: Jet aircraft engine exhaust emissions database development : year 1990 and 2015 scenarios (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Z. H. Landau and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets (National Aeronautics and Space Administration, 1963), also by Nickolai Charczenko and Clyde Hayes (page images at HathiTrust)
• Langley Research Center: Jet effects on cylindrical afterbodies housing sonic and supersonic nozzles which exhaust against a supersonic stream at angles of attack from 90 ̊to 180 ̊ (National Aeronautics and Space Administration, 1962), also by Lovick O. Hayman and Russell W. McDearmon (page images at HathiTrust)
• Langley Research Center: Jet effects on the drag of conical afterbodies at spersonic speeds (National Aeronautics and Space Administration ;, 1972), also by William B. Compton (page images at HathiTrust)
• Langley Research Center: Jet-engine exhaust noise from slot nozzles (National Aeronautics and Space Administration, 1959), also by Willard D. Coles (page images at HathiTrust)
• Langley Research Center: Jet transport flight operations using cockpit display of traffic information during instrument meteorological conditions : simulation evaluation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by David H. Williams and Douglas C. Wells (page images at HathiTrust)
• Langley Research Center: Joining and fabrication of metal-matrix composite materials (National Aeronautics and Space Administration ;, 1975), also by Dick M. Royster, Thomas T. Bales, and H. Ross Wiant (page images at HathiTrust)
• Langley Research Center: Joint design for improved fatigue life of diffusion-bonded box-stiffened panels (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Randall C. Davis, Russell S. Kanenko, and Paul L. Moses (page images at HathiTrust)
• Langley Research Center: Joint determination of orbits of spacecraft and moons of Mars by optical sighting of the moons (National Aeronautics and Space Administration ;, 1971), also by Charles B. Grosch, Donald F. Nickel, and Control Data Corporation (page images at HathiTrust)
• Langley Research Center: Joint University Program for Air Transportation Research, 1990-1991 : proceedings of a conference sponsored by the National Aeronautics and Space Administration, Washington, D.C., and the Federal Aviation Administration, Washington, D.C., and held in Athens, Ohio, June 20-21, 1991 (National Aeronautics and Space Administration, Office of Management, 1991), also by Frederick R. Morrell, United States Federal Aviation Administration, and United States. National Aeronautics and Space Administration. Office of Management (page images at HathiTrust; US access only)
• Langley Research Center: Kaon-nucleus scattering (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Byungsik Hong (page images at HathiTrust)
• Langley Research Center: Kinematic rate control of simulated robot hand at or near wrist singularity (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by L. Keith Barker, Susan W. Carzoo, and Jacob A. Houck (page images at HathiTrust)
• Langley Research Center: A kinetics investigation of several reactions involving chlorine containing compounds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Douglas D. Davis, University of Maryland, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Laboratory measurements of physical, chemical and optical characteristics of Lake Chicot sediment waters (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by William G. Witte and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A laboratory simulation of a single-axis dual-level precision pointing system (National Aeronautics and Space Administration ;, 1973), also by George F. Bullock, K. C. Romanczyk, Frederick R. Morrell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Laboratory studies of scales for measuring helicopter noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by J. B. Ollerhead, Wyle Laboratories, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Laboratory study of annoyance to combined airplane and road-traffic noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Clemans A. Powell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Laboratory tank studies of single species of phytoplankton using a remote sensing fluorosensor (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Clarence A. Brown, Franklin H. Farmer, Olin Jarrett, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Laboratory upwelled radiance and reflectance spectra of Kerr Reservoir sediment waters (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by William G. Witte and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Laminar flow transition : a large-eddy simulation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Sedat Biringen and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Laminar heat-transfer and pressure measurements at a Mach number of 6 on a sharp and blunt 15° half-angle cones at angles of attack up to 90° (National Aeronautics and Space Administration, 1961), also by Raul J. Conti and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Laminar heat-transfer distributions for a blunted-cone, cone-frustum reentry configuration at Mach 10 (National Aeronautics and Space Administration ;, 1969), also by J. David Dearing (page images at HathiTrust)
• Langley Research Center: Laminar or turbulent boundary-layer flows of perfect gases or reacting gas mixtures in chemical equilibrium (National Aeronautics and Space Administration ;, 1971), also by E. Clay Anderson, Clark H. Lewis, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Langley Research Center: The landing flare : an analysis and flight-test investigation (National Aeronautics and Space Administration ;, 1975), also by Edward Seckel and Princeton University. Flight Research Laboratory (page images at HathiTrust)
• Langley Research Center: Landing gear and cavity noise prediction (U.S. National Aeronautics and Space Administration ;, 1976), also by Donald B. Bliss, Richard E. Hayden, United States National Aeronautics and Space Administration, and Beranek Bolt (page images at HathiTrust)
• Langley Research Center: Landing-impact studies of a 0.3-scale model air cushion landing system for a Navy fighter airplane (National Aeronautics and Space Administration ;, 1975), also by Trafford J. W. Leland and William C. Thompson (page images at HathiTrust)
• Langley Research Center: Landing practices of general aviation pilots in single-engine light airplanes (National Aeronautics and Space Administration ;, 1976), also by Maxwell W. Goode and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The Langley 14- by 22-foot subsonic tunnel : description, flow characteristics, and guide for users (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Garl L. Gentry (page images at HathiTrust)
• Langley Research Center: Langley Atmospheric Information Retrieval System (LAIRS) : system description and user's guide (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by D. E. Boland, Taesul Lee, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Langley mach 4 scramjet test facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Earl H. Andrews (page images at HathiTrust)
• Langley Research Center: Langley Research Center. (National Aeronautics and Space Administration, Langley Research Center, 1990) (page images at HathiTrust)
• Langley Research Center: Large-area proton beams established at the NASA Space Radiation Effects Laboratory in the energy range from 31 to 225 MeV (National Aeronautics and Space Administration ;, 1970), also by Gerald Franklin Hill, William C. Honaker, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Large space antenna systems technology, 1982 (NASA, Scientific and Technical Information Branch, 1983), also by E. Burton Lightner and United States. Office of Aeronautics and Space Technology (page images at HathiTrust)
• Langley Research Center: Large space antenna systems technology, 1984 : proceedings of a conference (NASA, Scientific and Technical Information Branch ;, 1985), also by William J. Boyer and United States. Office of Aeronautics and Space Technology (page images at HathiTrust)
• Langley Research Center: Large space systems technology, 1980 : second annual technical review held at NASA Langley Research Center, Hampton, Virginia, November 18-20, 1980 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Frank Kopriver, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Large Space Systems Technology (LSST) Technical Review (2nd : 1980 : Langley Research Center) (page images at HathiTrust)
• Langley Research Center: Large space systems technology, 1981 : third annual technical review held at NASA Langley Research Center, Hampton, Virginia, November 16-19, 1981 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by William J. Boyer, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Large Space Systems Technology (LSST) Technical Review (3rd : 1981 : Langley Research Center) (page images at HathiTrust)
• Langley Research Center: Laser-powered MHD generators for space application (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by N. W. Jalufka (page images at HathiTrust)
• Langley Research Center: Laser production and heating of plasma for MHD application (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by N. W. Jalufka (page images at HathiTrust)
• Langley Research Center: Laser to single-mode-fiber coupling : a laboratory guide (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by I. Ladany and Lockheed Engineering & Sciences Company (page images at HathiTrust)
• Langley Research Center: Laser velocimeter (autocovariance) buffer interface (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by James I. Clemmons and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A laser velocimeter flow survey above a stalled wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Warren H. Young, Danny R. Hoad, James F. Meyers, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Laser velocimeter systems analysis applied to a flow survey above a stalled wing (National Aeronautics and Space Administration ;, 1977), also by Warren H. Young, Timothy E. Hepner, James F. Meyers, Langley Directorate, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Laser velocimetry technique applied to the Langley 0.3-Meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1981), also by Luther R. Gartrell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Lateral conduction effects on heat-transfer data obtained with the phase-change paint technique (National Aeronautics and Space Administration ;, 1974), also by George Maise, Michael J. Rossi, and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Arthur C. Grantz and Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept (page images at HathiTrust)
• Langley Research Center: Lateral directional stability characteristics at mach 2.3 to 3.5 of a supersonic transport model with various outboard vertical-tail locations (National Aeronautics and Space Administration ;, 1965), also by William A. Corlett (page images at HathiTrust)
• Langley Research Center: Lateral-directional stability characteristics of a wing-fuselage configuration at angles of attack up to 44 ̊ (National Aeronautics and Space Administration ;, 1974), also by William P. Henderson and Jarrett K. Huffman (page images at HathiTrust)
• Langley Research Center: The Lateral response of airplanes to random atmospheric turbulence (U.S. G.P.O., 1960), also by John M. Eggleston, William H. Phillips, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Lateral-spread sonic-boom ground-pressure measurements from airplanes at altitudes to 75,000 feet and at Mach numbers to 2.0 (National Aeronautics and Space Administration, 1963), also by Domenic J. Maglieri and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Lateral static and dynamic aerodynamic parameters of the Kestrel aircraft (XV-6A) extracted from flight data (National Aeronautics and Space Administration ;, 1974), also by William T. Suit and James L. Williams (page images at HathiTrust)
• Langley Research Center: Lateral vibration characteristics of the 1/10-scale Apollo/Saturn 5 replica model (National Aeronautics and Space Administration, 1970), also by Ellwood L. Peele, Sumner A. Leadbetter, H. Wayne Leonard, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Launch-vehicle dynamics (National Aeronautics and Space Administration, 1961), also by Harry L. Runyan and A. Gerald Rainey (page images at HathiTrust)
• Langley Research Center: Launch vehicle effluent measurements during the August 20, 1977, Titan III launch at Air Force Eastern Test Range (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by David C. Woods, Dewey E. Wornom, Richard J. Bendura, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Launch vehicle effluent measurements during the May 12, 1977, Titan III launch at Air Force Eastern Test Range (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Gerald L. Gregory, David C. Woods, Richard J. Bendura, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Launch vehicle integration options for a large earth sciences geostationary platform concept (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by James L. Garrison and Lawrence F. Rowell (page images at HathiTrust)
• Langley Research Center: LDEF Materials Workshop '91 : proceedings of a workshop (National Aeronautics and Space Administration, Langley Research Center, 1992), also by LDEF Materials Workshop (1991 : Langley Research Center), Philip R. Young, and Bland A. Stein (page images at HathiTrust)
• Langley Research Center: Lee-side flow over delta wings at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by David S. Miller and Richard M. Wood (page images at HathiTrust)
• Langley Research Center: LH2 Airport requirements study (U.S. National Aeronautics and Space Administration ;, 1976), also by United States National Aeronautics and Space Administration and Lockheed-California Company, ed. by G. D. Brewer (page images at HathiTrust)
• Langley Research Center: Lift and drag characteristics at subsonic speeds and at a Mach number of 1.9 of a lifting circular cylinder with a fineness ratio of 10 (National Aeronautics and Space Administration, 1959), also by Vernard E. Lockwood and Linwood W. McKinney (page images at HathiTrust)
• Langley Research Center: Lift generation on a circular cylinder by tangential blowing from surface slots (National Aeronautics and Space Administration, 1960), also by Vernard E. Lockwood (page images at HathiTrust)
• Langley Research Center: Light aircraft lift, drag, and moment prediction : a review and analysis (National Aeronautics and Space Administration, 1975), also by Frederick O. Smetana and North Carolina State University (page images at HathiTrust)
• Langley Research Center: Light airplane crash tests at three pitch angles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Victor L. Vaughan, Emilio Alfaro-Bou, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Light airplane crash tests at three roll angles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Claude B. Castle, Emilio Alfaro-Bou, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Lightning technology : proceedings of a technical symposium (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1980), also by Langley Research Center Symposium on Lightning Technology and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Lightning technology : proceedings of a technical symposium sponsored by the National Aeronautics and Space Administration, the Florida Institute of Technology, and the Department of Transportation and held at NASA Langley Research Center, Hampton, Virginia, April 22-24, 1980. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Florida Institute of Technology, United States. Department of Transportation, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, United States National Aeronautics and Space Administration, and Symposium on Lightning Technology (1980 : Langley Research Center) (page images at HathiTrust)
• Langley Research Center: Limb-darkening functions as derived from along-track operation of the ERBE scanning radiometers for August 1985 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by G. Louis Smith, Lee M. Avis, and Natividad D. Manalo (page images at HathiTrust)
• Langley Research Center: A limb radiance calculation approach for model atmospheres containing horizontal gradients of temperature and pressure (National Aeronautics and Space Administration, 1969), also by Richard E. Davis and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Wendell W. Kelley, Einar K. Enevoldson, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Hugh L. Dryden Flight Research Center (page images at HathiTrust)
• Langley Research Center: A limited flight and wind-tunnel investigation of paddle spoilers as lateral controls (National Aeronautics and Space Administration, 1959), also by Robert G. Mungall, William L. Alford, and Harold I. Johnson (page images at HathiTrust)
• Langley Research Center: The linear bicharacteristic scheme for electromagnetics (National Aeronautics and Space Administration, Langley Research Center, 2001), also by John H. Beggs (page images at HathiTrust)
• Langley Research Center: Linear systems analysis program, L224(QR). (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by K. W. Heidergott, P. C. Shah, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: The linear time optimal control problem from a calculus of variations point of view (National Aeronautics and Space Administration ;, 1970), also by Lawrence M. Hanafy and North Carolina State University (page images at HathiTrust)
• Langley Research Center: Linearity optimization in a class of analog phase modulators (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Chase P. Hearn (page images at HathiTrust)
• Langley Research Center: A linearly controlled direct-current power source for high-current inductive loads in a magnetic suspension wind tunnel (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by John S. Tripp and Taumi S. Daniels (page images at HathiTrust)
• Langley Research Center: Lithium-drifted silicon detectors as low-energy photon spectrometers (National Aeronautics and Space Administration ;, 1969), also by Sherwin M. Beck (page images at HathiTrust)
• Langley Research Center: Load concentration due to missing members in planar faces of a large space truss (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Joseph E. Walz and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Load interaction effects on fatigue crack growth in Ti-6Al-4V alloy (National Aeronautics and Space Administration ;, 1973), also by Robert Peh-ying Wei, J. H. FitzGerald, T. T. Shih, and Lehigh University (page images at HathiTrust)
• Langley Research Center: Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface (National Aeronautics and Space Administration, 1963), also by William Letko (page images at HathiTrust)
• Langley Research Center: Local stability analysis for a planar shock wave (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by M. D. Salas (page images at HathiTrust)
• Langley Research Center: Localized and distributed boundary-layer receptivity to convected unsteady wake in free stream (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Meelan Choudhari (page images at HathiTrust)
• Langley Research Center: Location of noise sources using a phase-slope method (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Richard DeLoach and John S. Preisser (page images at HathiTrust)
• Langley Research Center: Long duration exposure facility mini-data base user's guide : IBM-compatible PC computer version (National Aeronautics and Space Administration, Langley Research Center, 1995), also by G. L. Bohnhoff-Hlavacek, H. W. Dursch, and H. Gary Pippin (page images at HathiTrust)
• Langley Research Center: Long duration exposure facility mini-data base user's guide : Macintosh version (National Aeronautics and Space Administration, Langley Research Center, 1995), also by G. L. Bohnhoff-Hlavacek, H. W. Dursch, and H. Gary Pippin (page images at HathiTrust)
• Langley Research Center: Long-wavelength asymptotics of unstable crossflow modes, including the effect of surface curvature (National Aeronautics and Space Administration, Langley Research Center ;, 1994), also by Meelan Choudhari (page images at HathiTrust)
• Langley Research Center: Longitudinal aerodynamic characteristics and surface pressure measurements for a 1/10-scale model of the RAM B launch vehicle (National Aeronautics and Space Administration :, 1964), also by Thomas C. Kelly and Robert J. Keynton (page images at HathiTrust)
• Langley Research Center: Longitudinal aerodynamic characteristics at Mach 0.60 to 2.86 of a fighter configuration with strut braced wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Samuel M. Dollyhigh, Giuliana Sangiorgio, William J. Monta, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Longitudinal aerodynamic characteristics at Mach numbers from 0.50 to 1.19 of a supersonic transport model with a modified M wing (National Aeronautics and Space Administration ;, 1967), also by Edward J. Ray and Robert T. Taylor (page images at HathiTrust)
• Langley Research Center: Longitudinal aerodynamic characteristics at transonic speeds of a V/STOL airplane configuration with a fixed delta wing having auxiliary variable-sweep outboard panels (National Aeronautics and Space Administration, 1961), also by Arvo A. Luoma (page images at HathiTrust)
• Langley Research Center: Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings (National Aeronautics and Space Administration, 1961), also by Arvo A. Luoma (page images at HathiTrust)
• Langley Research Center: Longitudinal aerodynamic characteristics of a deflected-thrust propulsive-lift transport model (National Aeronautics and Space Administration ;, 1975), also by Danny R. Hoad (page images at HathiTrust)
• Langley Research Center: Longitudinal aerodynamic characteristics of a generic fighter model with a wing designed for sustained transonic maneuver conditions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by James C. Ferris (page images at HathiTrust)
• Langley Research Center: Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Laurence D. Leavitt and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Longitudinal aerodynamic characteristics of an elliptical body with a horizontal tail at mach numbers 2.3 to 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Barrett L. Shrout, A. Warner Robins, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Longitudinal aerodynamic characteristics of an externally blown flap powered-lift model with several propulsive system simulators (National Aeronautics and Space Administration ;, 1974), also by Danny R. Hoad (page images at HathiTrust)
• Langley Research Center: Longitudinal aerodynamic characteristics of two blunted cone reentry configurations at Mach numbers from 17.6 to 22.2 including some Reynolds number effects (National Aeronautics and Space Administration ;, 1966), also by Dal V. Maddalon (page images at HathiTrust)
• Langley Research Center: Longitudinal aerodynamic performance of a series of power-law and minimum-wave-drag bodies at Mach 6 and several Reynolds numbers (National Aeronautics and Space Administration ;, 1974), also by George C. Ashby (page images at HathiTrust)
• Langley Research Center: Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Peter F. Covell, Dorothy T. Howell, and Ira J. Walker (page images at HathiTrust)
• Langley Research Center: Longitudinal and lateral stability characteristics of two four-jet vtol models in the transition speed range (National Aeronautics and Space Administration, 1965), also by Raymond D. Vogler, Richard E. Kuhn, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Longitudinal stability and control derivatives of a jet fighter airplane extracted from flight test data by utilizing maximum likelihood estimation (National Aeronautics and Space Administration, 1971), also by George G. Steinmetz, Russell V. Parrish, Roland L. Bowles, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Longitudinal vibration characteristics of 1/10-scale Apollo/Saturn V replica model (National Aeronautics and Space Administration ;, 1969), also by Larry D. Pinson and H. Wayne Leonard (page images at HathiTrust)
• Langley Research Center: A loudness calculation procedure applied to shaped sonic booms (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Kevin P. Shepherd and Brenda M. Sullivan (page images at HathiTrust)
• Langley Research Center: Low-authority control synthesis for large space structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by J. N. Aubrun, G. Margulies, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Langley Research Center: Low-cycle fatigue evaluation for regeneratively cooled panels (National Aeronautics and Space Administration ;, 1971), also by C. E. Richard, AiResearch Manufacturing Company of Los Angeles (Calif.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Low Earth orbit thermal control coatings exposure flight tests : a comparison of U.S. and Russian results (National Aeronautics and Space Administration, Langley Research Center, 1995), also by A. C. Tribble (page images at HathiTrust)
• Langley Research Center: Low-energy electron effects on tensile modulus and infrared transmission properties of a polypyromellitimide film (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981), also by James E. Ferl, Edward R. Long, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Joint Institute for Advancement of Flight Sciences (page images at HathiTrust)
• Langley Research Center: A low energy electron magnetometer (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Jag J. Singh and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Low-energy gamma ray attenuation characteristics of aviation fuels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Jag J. Singh, Danny R. Sprinkle, and Chih-Ping Shen (page images at HathiTrust)
• Langley Research Center: Low-energy positron flux generator for microstructural characterization of thin films (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Jag J. Singh, Terry L. St. Clair, and Abe Eftekhari (page images at HathiTrust)
• Langley Research Center: Low power, compact charge coupled device signal processing system (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, P. W. Bosshart, and Texas Instruments Incorporated (page images at HathiTrust)
• Langley Research Center: Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and sideslip (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Raymond D. Whipple and Jonathan L. Ricket (page images at HathiTrust)
• Langley Research Center: Low-speed aerodynamic characteristics of a 16-percent thick variable-geometry airfoil designed for general aviation applications (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Richard W. Barnwell, Robert J. McGhee, Kevin W. Noonan, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Low-speed aerodynamic characteristics of a transport model having 42.33 ̊swept low wing with supercritical airfoil, double-slotted flaps, and T-tail or low tail (National Aeronautics and Space Administration ;, 1975), also by Paul G. Fournier (page images at HathiTrust)
• Langley Research Center: Low speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by Dana Morris Dunham (page images at HathiTrust)
• Langley Research Center: Low-speed aerodynamic characteristics of airfoil sections with rounded trailing edges in forward and reverse flow (National Aeronautics and Space Administration ;, 1974), also by William D. Beasley and Robert J. McGhee (page images at HathiTrust)
• Langley Research Center: Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient (National Aeronautics and Space Administration ;, 1972), also by Gene J. Bingham and Allen Wen-shin Chen (page images at HathiTrust)
• Langley Research Center: Low speed aerodynamic characteristics of NACA 6716 and NACA 4416 airfoils with 35 percent-chord single-slotted flaps (National Aeronautics and Space Administration ;, 1974), also by Gene J. Bingham and Kevin W. Noonan (page images at HathiTrust)
• Langley Research Center: Low-speed characteristics of a variable-sweep supersonic transport model with a blended engine fuselage and engine-mounted tails (National Aeronautics and Space Administration, 1964), also by Vernard E. Lockwood and Wilson E. Thompson (page images at HathiTrust)
• Langley Research Center: Low-speed effects of high-lift devices on the aerodynamic characteristics of a supersonic transport model with outboard tails (National Aeronautics and Space Administration, 1963), also by William C. Sleeman, Paul G. Fournier, and Edward J. Ray (page images at HathiTrust)
• Langley Research Center: Low-speed free-flight stability and drag characteristics of radially vented parachutes (NASA :, 1964), also by Sanger M. Burk and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Gregory M. Gatlin (page images at HathiTrust)
• Langley Research Center: Low-speed investigation of effects of vertical tails on the static stability characteristics of a canard-bomber configuration having a very thin wing and a slender elliptical fuselage (National Aeronautics and Space Administration, 1961), also by Thomas G. Gainer (page images at HathiTrust)
• Langley Research Center: Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body (National Aeronautics and Space Administration, 1961), also by William C. Sleeman and A. Warner Robins (page images at HathiTrust)
• Langley Research Center: Low-speed longitudinal stability characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot (National Aeronautics and Space Administration, 1961), also by William P. Henderson (page images at HathiTrust)
• Langley Research Center: Low-speed measurements of oscillatory lateral stability derivatives of a model of 60 degree delta-wing bomber (National Aeronautics and Space Administration, 1959), also by John W. Paulson (page images at HathiTrust)
• Langley Research Center: Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Zachary T. Applin and Paul L. Coe (page images at HathiTrust)
• Langley Research Center: Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Dale R. Satran, Ernie L. Anglin, and William P. Gilbert (page images at HathiTrust)
• Langley Research Center: Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by David E. Hahne (page images at HathiTrust)
• Langley Research Center: Low-speed static wind-tunnel investigation of a half-span fuselage and variable-sweep pressure wing model (National Aeronautics and Space Administration, 1971), also by John E. Lamar, L. Wayne McKinney, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A low speed two-dimensional study of flow separation on the GA(W)-1 airfoil with 30-percent chord Fowler flap (National Aeronautics and Space Administration, 1977), also by H. C. Seetharam, W. H. Wentz, and Wichita State University (page images at HathiTrust)
• Langley Research Center: Low-speed upwash interference on a transport model in a rectangular slotted-wall wind tunnel (National Aeronautics and Space Administration ;, 1975), also by Michael J. Mann (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel investigation of a four-engine upper surface blown model having a swept wing and rectangular and D-shaped exhaust nozzles (National Aeronautics and Space Administration ;, 1975), also by William C. Sleeman and William C. Hohlweg (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings (National Aeronautics and Space Administration ;, 1970), also by Roger L. Naeseth (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel investigation of a swept-wing model having distributed upper-surface blowing near the wing leading edge or at the flap knee (National Aeronautics and Space Administration ;, 1977), also by William C. Sleeman, United States National Aeronautics and Space Administration, and David R Forsyth (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel investigation of a wingless jet VTOL transport model (National Aeronautics and Space Administration, 1959), also by Marion O. McKinney (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel investigation of flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Paul L. Coe, D. B. Owens, and Steven G. Turner (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel investigation of flight spoilers as trailing-vortex-alleviation devices on an extended-range wide-body tri-jet airplane model (National Aeronautics and Space Administration ;, 1976), also by Delwin R. Croom, John A. Thelander, Raymond D. Vogler, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel investigation of forward-located spoilers and trailing splines as trailing-vortex hazard-alleviation devices on an aspect-ratio-8 wing model (National Aeronautics and Space Administration ;, 1975), also by Delwin R. Croom (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel investigation of span load alteration, forward-located spoilers, and splines as trailing-vortex-hazard alleviation devices on a transport aircraft model (National Aeronautics and Space Administration ;, 1975), also by Delwin R. Croom and R. Earl Dunham (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Jay M. Brandon (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel investigation of various segments of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model (U.S. National Aeronautics and Space Administration, Langley Research Center ;, 1976), also by Delwin R. Croom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel investigation of wing fins as trailings-vortex-alleviation devices on a transport airplane model (National Aeronatutics and Space Administration, Scientific and Technical Information Branch :, 1979), also by Delwin R. Croom, G. Thomas Holbrook, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel parametric investigation of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Delwin R. Croom and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Donald R. Riley, Gautam H. Shah, and Richard E. Kuhn (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Michael B. Lance, Robert H. Stroub, and Daniel Y. Sung (page images at HathiTrust)
• Langley Research Center: Low-speed wind-tunnel tests of an advanced eight-bladed propeller (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Paul L. Coe, Dana Morris Dunham, and Garl L. Gentry (page images at HathiTrust)
• Langley Research Center: Low subsonic flight and force investigation of a supersonic transport model with a double-delta wing (National Aeronautics and Space Administration, 1968), also by Delma C. Freeman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Low subsonic flight and force investigation of a supersonic transport model with a highly swept arrow wing (National Aeronautics and Space Administration, 1967), also by Delma C. Freeman (page images at HathiTrust)
• Langley Research Center: Low subsonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading-edge sweep (National Aeronautics and Space Administration, 1961), also by Paul G. Fournier, B. Ann Bell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Low-temperature forming of beta titanium alloys (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by R. S. Kaneko, C. A. Woods, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Low-temperature solder for joining large cryogenic structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John D. Buckley, Paul G. Sandefur, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Lowspeed wind-tunnel investigation of a semispan STOL jet transport wing-body with an upper-surface blown jet flap (National Aeronautics and Space Administration ;, 1973), also by Arthur R. Phelps, Robert L. Henderson, and William Letko (page images at HathiTrust)
• Langley Research Center: LSST (Hoop/Column) Maypole antenna development program (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1982), also by Marvin R. Sullivan, Harris Corporation. Electronic Systems, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Luminous efficiencies of three nickel artificial meteors between 9.8 and 11.4 kilometers per second (National Aeronautics and Space Administration ;, 1968), also by T. Dale Bess and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A lunar gravity simulator. (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), also by Case Western Reserve University, Dennis A. Millett, Richard J. Morgan, and Case Institute of Technology (page images at HathiTrust)
• Langley Research Center: Lunar orbiter I : extended-mission spacecraft subsystem performance. (National Aeronautics and Space Administration ;, 1967), also by Boeing Company (page images at HathiTrust)
• Langley Research Center: Lunar Orbiter I : photographic mission summary (National Aeronautics and Space Administration, 1967), also by Boeing Company and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Lunar orbiter I : postmission photo supporting data (Boeing, 1967), also by Boeing Company (page images at HathiTrust)
• Langley Research Center: Lunar orbiter II : postmission photo supporting data (Boeing, 1967), also by Boeing Company (page images at HathiTrust)
• Langley Research Center: Lunar Orbiter III : Extended-Mission spacecraft operations and subsystem performance. (National Aeronautics and Space Administration ;, 1968), also by Boeing Company and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Lunar orbiter III : postmission photo supporting data (Boeing, 1967), also by Boeing Company (page images at HathiTrust)
• Langley Research Center: Lunar Orbiter IV. Photographic mission summary. (National Aeronautics and Space Administration ;, 1968), also by Boeing Company (page images at HathiTrust)
• Langley Research Center: Lunar orbiter IV : postmission photo supporting data (Boeing, 1967), also by Boeing Company (page images at HathiTrust)
• Langley Research Center: Lunar orbiter V : photography (National Aeronautics and Space Administration, 1968), also by Boeing Company and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Lunar orbiter V : postmission photo supporting data (Boeing, 1967), also by Boeing Company (page images at HathiTrust)
• Langley Research Center: Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65⁰ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Edward R. Hartman and Patrick J. Johnston (page images at HathiTrust)
• Langley Research Center: Mach 6 flow field surveys beneath the forebody of an airbreatinng missile (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Patrick J. Johnston and James L. Hunt (page images at HathiTrust)
• Langley Research Center: Magnetic ignition of pulsed gas discharges in air of low pressure in a coaxial plasma gun (National Aeronautics and Space Administration, 1961), also by Karlheinz Thom and Joseph Norwood (page images at HathiTrust)
• Langley Research Center: Magnetic suspension and balance system advanced study (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by R. W. Boom and Inc Madison Magnetics (page images at HathiTrust)
• Langley Research Center: Magnetic suspension and balance system advanced study, phase II (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by R. W. Boom and Inc Madison Magnetics (page images at HathiTrust)
• Langley Research Center: Magnetic suspension and balance system study (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by R. W. Boom and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Magnetic suspension and balance systems : a comprehensive, annotated bibliography (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Marie H. Tuttle, Robert A. Kilgore, and Deborah L. Moore (page images at HathiTrust)
• Langley Research Center: Magnetic suspension and balance systems : a selective annotated bibliography (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1980), also by Marie H. Tuttle, Richmond P. Boyden, and Robert A. Kilgore (page images at HathiTrust)
• Langley Research Center: Main rotor free wake geometry effects on blade air loads and response for helicopters in steady maneuvers (National Aeronautics and Space Administration ;, 1972), also by S. Gene Sadler and Rochester Applied Sciences Associates (page images at HathiTrust)
• Langley Research Center: Making statistical inferences about software reliability (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Douglas R. Miller (page images at HathiTrust)
• Langley Research Center: Maneuver and buffet characteristics of fighter aircraft (National Aeronautics and Space Administration ;, 1973), also by Edward J. Ray, Julian G. Carmichael, and Linwood W. McKinney (page images at HathiTrust)
• Langley Research Center: Manual-control simulation study of a nonlifting vehicle during orbit, retro-rocket firing, and reentry into the earth's atmosphere (National Aeronautics and Space Administration, 1960), also by Roger M. Davidson, Jack T. Kaylor, and Donald C. Cheatham (page images at HathiTrust)
• Langley Research Center: A marching method for calculating line and continuum radiation in high energy flow fields (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Charles W. Bolz and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Marking parts to aid robot vision (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John W. Bales, L. Keith Barker, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Mars gravitational field estimation error (National Aeronautics and Space Administration ;, 1972), also by Harold R. Compton and Edward F. Daniels (page images at HathiTrust)
• Langley Research Center: Mass distribution of orbiting man-made space debris (National Aeronautics and Space Administration ;, 1975), also by T. Dale Bess (page images at HathiTrust)
• Langley Research Center: Mass flux similarity for slotted transonic-wind-tunnel walls (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Joel L. Everhart and Suresh H. Goradia (page images at HathiTrust)
• Langley Research Center: Mass loss of a TEOS-coated, reinforced carbon-carbon composite subjected to a simulated shuttle entry environment (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1981), also by C. W. Stroud, Donald R. Rummler, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Mass spectrometric gas composition measurements associated with jet interaction tests in a high-enthalpy wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Beverley W. Lewis (page images at HathiTrust)
• Langley Research Center: Mass transfer cooling near the stagnation point (U.S. G.P.O., 1959), also by Leonard Roberts and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Material characterization of superplastically formed titanium (Ti-6Al-2Sn-4Zr-2Mo) sheet (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by William A. Ossa and Dick M. Royster (page images at HathiTrust)
• Langley Research Center: A material selection method based on material properties and operating parameters (National Aeronautics and Space Administration ;, 1973), also by Wolf Elber, John R. Davidson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A mathematical model of an active control landing gear for load control during impact and roll-out (National Aeronautics and Space Administration ;, 1976), also by John R. McGehee and Huey D. Carden (page images at HathiTrust)
• Langley Research Center: Mathematical modeling of damage in unidirectional composites (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1981), also by J. G. Goree, Walter F. Jones, Lokeswarappa R. Dharani, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A matrix method for studying motions of spacecraft consisting of interconnected rigid bodies (National Aeronautics and Space Administration ;, 1968), also by Richard E. Turner and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Maximum likelihood identification and optimal input design for identifying aircraft stability and control derivatives (National Aeronautics and Space Administration ;, 1973), also by David E. Stepner, Raman K. Mehra, and inc Systems Control (page images at HathiTrust)
• Langley Research Center: Maximum likelihood method for estimating airplane stability and control parameters from flight data in frequency domain (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Vladislav Klein and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Mean-flow and turbulence measurements in the vicinity of the trailing edge of an NACA 63₁-012 airfoil (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by James C. Yu and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Mean velocities and Reynolds stresses in a juncture flow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by H. McMahon, J. Hubbartt, L. Kubendran, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Georgia Institute of Technology (page images at HathiTrust)
• Langley Research Center: Measured and calculated acoustic attenuation rates of tuned resonator arrays for two surface impedance distribution models with flow (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Tony L. Parrott, Michael G. Jones, and A. Louis Abrahamson (page images at HathiTrust)
• Langley Research Center: Measured and calculated neutron spectra and dose equivalent rates at high altitudes : relevance to SST operations and space research (National Aeronautics and Space Administration ;, 1974), also by Trutz Foelsche (page images at HathiTrust)
• Langley Research Center: Measured and calculated transmission losses of sound waves through a helium layer (National Aeronautics and Space Administration ;, 1973), also by Thomas D. Norum and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Measured and predicted aerodynamic coefficients and shock shapes for Aeroassist Flight Experiment (AFE) configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by William L. Wells (page images at HathiTrust)
• Langley Research Center: Measured and predicted section wave drag coefficients at a Mach number of 1.6 for a delta wing with two airfoil sections (National Aeronautics and Space Administration, 1959), also by Frederick C. Grant (page images at HathiTrust)
• Langley Research Center: Measured human transfer functions in simulated single-degree-of-freedom nonlinear control systems (National Aeronautics and Space Administration :, 1965), also by Hugh P. Bergeron, James J. Adams, and Joseph King Kincaid (page images at HathiTrust)
• Langley Research Center: Measured opening characteristics of an electromagnetically opened diaphragm for the Langley expansion tunnel (U.S. National Aeronautics and Space Administration ;, 1976), also by John A. Moore and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Measured pressure distributions, aerodynamic coefficients, and shock shapes on blunt bodies at incidence in hypersonic air and CF₄ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), also by Charles G. Miller and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Measured pressure distributions on large-angle cones in hypersonic flows of tetrafluoromethane, air, and helium (National Aeronautics and Space Administration ;, 1973), also by Robert A. Jones and James L. Hunt (page images at HathiTrust)
• Langley Research Center: Measured transfer functions of pilots during two-axis tasks with motion (National Aeronautics and Space Administration :, 1964), also by Hugh P. Bergeron and James J. Adams (page images at HathiTrust)
• Langley Research Center: Measured variation in the transfer function of a human pilot in single-axis tasks (National Aeronautics and Space Administration, 1963), also by James J. Adams and Hugh P. Bergeron (page images at HathiTrust)
• Langley Research Center: Measured vibration response characteristics of four residential structures excited by mechanical and acoustical loadings (National Aeronautics and Space Administration ;, 1970), also by Huey P. Carden, William C. Mayes, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Measurement and analysis of aircraft far-field aerodynamic noise (National Aeronautics and Space Administration ;, 1974), also by Gerald J. Healy and Lockheed-California Company (page images at HathiTrust)
• Langley Research Center: Measurement of aerodynamic heat transfer to a deflected trailing-edge flap on a delta fin in free flight at Mach numbers from 1.5 to 2.6 (National Aeronautics and Space Administration, 1960), also by Leo T. Chauvin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Measurement of fault latency in a digital avionic mini processor (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John G. McGough, Fred L. Swern, Bendix Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Measurement of flow angularity at supersonic and hypersonic speeds with the use of a conical probe (National Aeronautics and Space Administration, 1961), also by Frank E. Swalley and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Measurement of operator workload in an information processing task (National Aeronautics and Space Administration ;, 1972), also by Larry L. Jenney, Bernard J. Cameron, Harry J. Older, and inc Biotechnology (page images at HathiTrust)
• Langley Research Center: Measurement of SIFT operating system overhead (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Daniel L. Palumbo and Ricky W. Butler (page images at HathiTrust)
• Langley Research Center: Measurement of the errors of service altimeter installations during landing-approach and take-off operations (National Aeronautics and Space Administration :, 1960), also by William Gracey, Gene T. Carpenter, and Joseph W. Jewel (page images at HathiTrust)
• Langley Research Center: Measurement of velocity and vorticity fields in the wake of an airfoil in periodic pitching motion (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by Earl R. Booth (page images at HathiTrust)
• Langley Research Center: Measurement techniques and applications of charge transfer to aerospace research (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Alphonsa Smith and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Measurement techniques investigated for detection of hydrogen chloride gas in ambient air (National Aeronautics and Space Administration ;, 1976), also by Gerald L. Gregory and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Measurements of dielectric constants and loss tangents at E-band using a Fabry-Perot interferometer. (National Aeronautics and Space Administration, 1969), also by Constantine A. Balanis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Measurements of farfield sound generation from a flow-excited cavity (National Aeronautics and Space Administration ;, 1975), also by P. J. W. Block and H. Heller (page images at HathiTrust)
• Langley Research Center: Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 (National Aeronautics and Space Administration, 1959), also by Harry W. Carlson (page images at HathiTrust)
• Langley Research Center: Measurements of flow rate and trajectory of aircraft tire-generated water spray (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Robert H. Daugherty and Sandy M. Stubbs (page images at HathiTrust)
• Langley Research Center: Measurements of fluctuating pressure in a rectangular cavity in transonic flow at high Reynolds numbers (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by M. B. Tracy, Julio Chu, and Elizabeth B. Plentovich (page images at HathiTrust)
• Langley Research Center: Measurements of forces, moments, and pressures on a generic store separating from a box cavity at supersonic speeds (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Robert L. Stallings, Dana K. Forrest, and Floyd J. Wilcox (page images at HathiTrust)
• Langley Research Center: Measurements of pressure on the tail and aft fuselage of an airplabne model during rotary motions at spin attitudes (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by James S. Bowman, Colin A. Martin, and Randy S. Hultberg (page images at HathiTrust)
• Langley Research Center: Measurements of the dielectric properties of sea water at 1.43 Ghz (National Aeronautics and Space Administration, 1974), also by W. W. Ho, M. J. Van Melle, A. W. Love, United States National Aeronautics and Space Administration, and Rockwell International (page images at HathiTrust)
• Langley Research Center: Measurements of the surface flows, heat transfer, pressure distribution, and longitudinal stability of a mercury capsule model at Mach numbers of 6.9 and 9.6 (National Aeronautics and Space Administration, 1961), also by Philip E. Everhart and Peter T. Bernot (page images at HathiTrust)
• Langley Research Center: Measurements of winds and temperatures at altitudes up to 65 kilometers in the Southern Hemisphere (National Aeronautics and Space Administration, 1968), also by James C. Manning, Lloyd W. Chamberlain, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Mechanical properties and column behavior of thin-wall Be-38Al alloy tubing (National Aeronautics and Space Administration ;, 1969), also by Donald R. Rummler (page images at HathiTrust)
• Langley Research Center: Mechanical properties of LaRC [superscript TM] SI polymer for a range of molecular weights (National Aeronautics and Space Administration, Langley Research Center, 2000), also by Karen S. Whitley (page images at HathiTrust)
• Langley Research Center: Mechanical property characterization of Borsic®/aluminum laminates at room and elevated temperatures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Robert R. McWithey, Dick M. Royster, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Mechanics of Textile Composites Conference : proceedings of a conference sponsored by the National Aeronautics and Space Administration, Washington, D.C., and held in Hampton, Va., December 6-8, 1994 (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by Va.) Mechanics of Textile Composites Conference (1994 : Hampton, Charles E. Harris, C. C. Poe, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Mesoscale acid deposition modeling studies (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Michael L. Kaplan and Inc MESO (page images at HathiTrust)
• Langley Research Center: Meteor research program (National Aeronautics and Space Administration ;, 1972), also by A. F. Cook and Smithsonian Astrophysical Observatory (page images at HathiTrust)
• Langley Research Center: Meteoroid bumper experiment on Explorer 46 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Donald H. Humes and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Meteorological rocket research since 1959 and current requirements for observations and analysis above 60 kilometers (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1969), also by Roderick S. Quiroz and Suitland United States. National Meteorological Center (page images at HathiTrust; US access only)
• Langley Research Center: A method for analyzing dynamic stall of helicopter rotor blades (National Aeronautics and Space Administration ;, 1972), also by Peter Crimi, Barry L. Reeves, and Avco Corporation (page images at HathiTrust)
• Langley Research Center: A method for analyzing the aeroelastic stability of a helicopter rotor in forward flight (National Aeronautics and Space Administration ;, 1969), also by Peter Crimi and Applied Science Associates (page images at HathiTrust)
• Langley Research Center: A method for calculating a real-gas two-dimensional nozzle contour including the effects of gamma (National Aeronautics and Space Administration ;, 1975), also by Charles B. Johnson and Lillian R. Boney (page images at HathiTrust)
• Langley Research Center: A method for calculating aerodynamic loadings on thin wings at a Mach number of 1 (National Aeronautics and Space Administration, 1959), also by John L. Crigler (page images at HathiTrust)
• Langley Research Center: A method for calculating the aerodynamic loading on wing-body combinations at small angles of attack in supersonic flow (National Aeronautics and Space Administration, 1971), also by Charlie M. Jackson, Wallace C. Sawyer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A method for calibration of gas-composition-sensitive pressure gages in condensible vapors (National Aeronautics and Space Administration :, 1965), also by Leonard T. Melfi and Paul R. Yeager (page images at HathiTrust)
• Langley Research Center: A method for computation of vibration modes and frequencies of orthotropic thin shells of revolution having general meridional curvature (National Aeronautics and Space Administration, 1969), also by Howard M. Adelman, William C. Walton, Donnell S. Catherines, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A method for computing the leading-edge suction in a higher-order panel method (National Aeronautical and Space Administration, Scientific and Technical Information Office ;, 1984), also by F. Edward Ehlers, Marjorie E. Manro, Boeing Commercial Airplane Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A method for determining acoustic-liner admittance in ducts with sheared flow in two cross-sectional directions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Willie R. Watson (page images at HathiTrust)
• Langley Research Center: A method for determining local elastoplastic stress and strain in metallurgically bonded notched laminates subjected to a loading cycle (National Aeronautics and Space Administration ;, 1974), also by J. A. Sova and John H. Crews (page images at HathiTrust)
• Langley Research Center: A method for determining optimum phasing of a multiphase propulsion system for a single-stage vehicle with linearized inert weight (National Aeronautics and Space Administration ;, 1974), also by James A. Martin (page images at HathiTrust)
• Langley Research Center: A method for estimating some longitudinal and lateral rigid-body responses of airplanes to continuous atmospheric turbulence (National Aeronautics and Space Administration, 1971), also by Ellwood L. Peele and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A method for longitudinal and lateral range control for a high-drag low-lift vehicle entering the atmosphere of a rotating earth (National Aeronautics and Space Administration, 1961), also by John W. Young and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A method for obtaining practical flutter-suppression control laws using results of optimal control theory (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Jerry R. Newsom and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A Method for obtaining reduced-order control laws for high-order systems using optimization techniques (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Vivek Mukhopadhyay, Irving Abel, Jerry R. Newsom, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A method for predicting the noise levels of coannular jets with inverted velocity profiles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by James W. Russel and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A method for the design of transonic flexible wings (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Leigh Ann Smith and Richard L. Campbell (page images at HathiTrust)
• Langley Research Center: A method for the measurement and analysis of ride vibrations of transportation systems (National Aeronautics and Space Administration, 1972), also by Harland F. Scholl, Sherman A. Clevenson, John J. Catherines, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A method of automatically stabilizing helicopter sling loads (National Aeronautics and Space Administration ;, 1974), also by Joseph Gera and Steve W. Farmer (page images at HathiTrust)
• Langley Research Center: A method of integral relations solution for radiating, nonadiabatic, inviscid flow over a blunt body (National Aeronautics and Space Administration ;, 1969), also by John T. Suttles (page images at HathiTrust)
• Langley Research Center: A method of limit point calculation in finite element structural analysis (National Aeronautics and Space Administration ;, 1972), also by Richard H. Gallagher, S. T. Mau, and Cornell University (page images at HathiTrust)
• Langley Research Center: A method of slitless absolute spectral photometry (National Aeronautics and Space Administration ;, 1967), also by Gale A. Harvey and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A method to stabilize linear systems using Eigenvalue gradient information (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Carol D. Wieseman (page images at HathiTrust)
• Langley Research Center: A methodology for boost-glide transport technology planning (National Aeronautics and Space Administration ;, 1974), also by E. M. Repic, R. J. Milliken, G. A. Olson, and Rockwell International. Space Division (page images at HathiTrust)
• Langley Research Center: A methodology for computing uncertainty bounds of multivariable systems based on sector stability theory concepts (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Martin R. Waszak (page images at HathiTrust)
• Langley Research Center: A methodology for designing aircraft to low sonic boom constraints (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Robert J. Mack and Kathy E. Needleman (page images at HathiTrust)
• Langley Research Center: Methods for determining the optimum design of structures protected from aerodynamic heating and application to typical boost-glide or reentry flight paths (National Aeronautics and Space Administration, 1962), also by Robert S. Harris, John R. Davidson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Methods for estimating pressure and thermal loads induced by elevon deflections on hypersonic-vehicle surfaces with turbulent boundary layers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Louis G. Kàufman, Charles B. Johnson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: The methods of paired comparisons and magnitude estimation in judging the noisiness of aircraft (National Aeronautics and Space Administration ;, 1972), also by Frank R. Clarke, Karl D. Kryter, and Stanford Research Institute (page images at HathiTrust)
• Langley Research Center: Microcracking, microcrack-induced delamination, and longitudinal splitting of advanced composite structures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by John A. Nairn, University of Utah, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: Micromechanics of fatigue in woven and stitched composites (National Aeronautics and Space Administration, Langley Research Center ;, 1994), also by B. N. Cox and Rockwell International. Science Center (page images at HathiTrust)
• Langley Research Center: A microprocessor-based table lookup approach for magnetic bearing linearization (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Nelson J. Groom, James B. Miller, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Microwave spectra of some chlorine and fluorine compounds (National Aeronautics and Space Administration ;, 1975), also by William F. White (page images at HathiTrust)
• Langley Research Center: Microwave spectra of some sulfur and nitrogen compounds (National Aeronautics and Space Administration ;, 1974), also by William F. White (page images at HathiTrust)
• Langley Research Center: Microwave spectra of some volatile organic compounds (National Aeronautics and Space Administration ;, 1975), also by William F. White (page images at HathiTrust)
• Langley Research Center: Midcourse-guidance procedure with single position fix obtained from onboard optical measurements (National Aeronautics and Space Administration ;, 1967), also by Harold A. Hamer, W. Thomas Blackshear, and Katherine G. Johnson (page images at HathiTrust)
• Langley Research Center: Mikhailov stability criterion for time-dalayed systems (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by L. Keith Barker and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Miniature flow-direction and airspeed sensor for airplanes and radio-controlled models in spin studies (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by David D. Kershner and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Minimization theory of induced drag subject to constraint conditions (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by John DeYoung and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Minimum fuel ascent from the lunar surface (National Aeronautics and Space Administration ;, 1967), also by Albert E. Brown (page images at HathiTrust)
• Langley Research Center: Minimum-mass design of filamentary composite panels under combined loads : design procedure based on a rigorous buckling analysis (National Aeronautics and Space Administration ;, 1977), also by W. Jefferson Stroud, Melvin S. Anderson, Nancy Agranoff, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Minimum-weight analysis of symmetrical-multiweb-beam structures subjected to thermal stress (National Aeronautics and Space Administration, 1959), also by Robert R. McWithey (page images at HathiTrust)
• Langley Research Center: Minimum weight design of axially compressed ring and stringer stiffened cylindrical shells (National Aeronautics and Space Administration ;, 1971), also by David L. Block and Florida Technological University (page images at HathiTrust)
• Langley Research Center: Minimum weight design of ring and stringer stiffeners for axially compressed cylindrical shells with and without internal pressure (National Aeronautics and Space Administration ;, 1972), also by David L. Block and Florida Technological University (page images at HathiTrust)
• Langley Research Center: Minimum-weight designs for hat-stiffened composite panels under uniaxial compression (National Aeronautics and Space Administration ;, 1974), also by Banarsi Agarwal and Randall C. Davis (page images at HathiTrust)
• Langley Research Center: MIRACAL : a mission radiation calculation program for analysis of lunar and interplanetary missions (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by John E. Nealy, Lisa C. Simonsen, and Scott A. Striepe (page images at HathiTrust)
• Langley Research Center: Mission description and in-flight operations of ERBE instruments on ERBS and NOAA 9 spacecraft : November 1984 through January 1986 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by William L. Weaver (page images at HathiTrust)
• Langley Research Center: Mitotic synchronization of L-strain fibroblasts wuth 5-aminouracil as determined by time-lapse cinephotography (National Aeronautics and Space Administration ;, 1969), also by Clarence D. Cone and Max Tongier (page images at HathiTrust)
• Langley Research Center: Mixing-height measurement by lidar, particle counter, and rawinsonde in the Willamette Valley, Oregon (National Aeronautics and Space Administration ;, 1972), also by M. Patrick McCormick (page images at HathiTrust)
• Langley Research Center: Mixing of hydrogen injected from multiple injectors normal to a supersonic airstream (National Aeronautics and Space Administration :, 1971), also by R. Clayton Rogers and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Modal control theory and application to aircraft lateral handling qualities design (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by S. Srinathkumar and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Modal interaction in postbuckled plates : theory (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Gaylen A. Thurston (page images at HathiTrust)
• Langley Research Center: Model-based reconfiguration : diagnosis and recovery (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Judy Crow and John Rushby (page images at HathiTrust)
• Langley Research Center: A model-based technique for predicting pilot opinion ratings for large commercial transporters (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by William H. Levison, Beranek Bolt, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A model for jet-noise analysis using pressure-gradient correlations on an imaginary cone (National Aeronautics and Space Administration ;, 1974), also by Thomas D. Norum (page images at HathiTrust)
• Langley Research Center: Model reduction by trimming for a class of semi-Markov reliability models and the corresponding error bound (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Allan L. White (page images at HathiTrust)
• Langley Research Center: Model tests of jet-induced lift effects on a VTOL aircraft in hover (National Aeronautics and Space Administration ;, 1969), also by P. K. Shumpert, J. G. Tibbetts, Lockheed-Georgia Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Modeling and analysis of the space shuttle nose-gear tire with semianalytic finite elements (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Kyun O. Kim, John A. Tanner, and Ahmed Khairy Noor (page images at HathiTrust)
• Langley Research Center: Modeling of joints for the dynamic analysis of truss structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by W. Keith Belvin (page images at HathiTrust)
• Langley Research Center: Models and measurements intercomparison two (National Aeronautics and Space Administration, Langley Research Center, 1999), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Modification and validation of conceptual design aerodynamic prediction method HASC95 with VTXCHN (National Aeronautics and Space Administration, 1996), also by Alan E. Albright, Martin C. Hegedus, Charles J. Dixon, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by T. C. Corke, Hassan M. Nagib, Y. Guezennec, Illinois Institute of Technology, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Modification of an impulse-factoring orbital-transfer technique to account for orbit-determination and maneuver-execution errors (National Aeronautics and Space Administration ;, 1974), also by James F. Kibler (page images at HathiTrust)
• Langley Research Center: Modifications to the nozzle test chamber to extend nozzle static-test capability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by J. Wayne Keyes (page images at HathiTrust)
• Langley Research Center: A modificiation to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attack (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Harry W. Carlson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Modified Denavit-Hartenberg parameters for better location of joint axis systems in robot arms (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by L. Keith Barker (page images at HathiTrust)
• Langley Research Center: A modified Newton-Raphson analysis of flight measurements of the trailing vortices of a heavy jet transport (National Aeronautics and Space Administration ;, 1974), also by Lawrence W. Taylor and Milton D. McLaughlin (page images at HathiTrust)
• Langley Research Center: A modified Theodorsen [epsilon]-function airfoil design procedure (National Aeronautics and Space Administration ;, 1974), also by Raymond L. Barger (page images at HathiTrust)
• Langley Research Center: Modular antenna design study (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John W. Ribble and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Modular reflector concept study (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by D. H. Vaughan and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Modulated entry (National Aeronautics and Space Administration :, 1960), also by Frederick C. Grant (page images at HathiTrust)
• Langley Research Center: Modulated infrared radiant source (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by W. F. Stewart and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Moisture determination in composite materials using positron lifetime technique (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Jag J. Singh, Willis Mock, William H. Holt, Naval Surface Weapons Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Moisture diffusion parameter characteristics for epoxy composites and neat resins (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Edward R. Long and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Molecular orientation and mechanical anisotropy in polyethylene, polypropylene, and poly(ethylene terephthalate) films (National Aeronautics and Space Administration ;, 1969), also by Howard L. Price and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A momentum analysis of helicopters and autogyros in inclined descent, with comments on operational restrictions (National Aeronautics and Space Administration ;, 1975), also by Harry H. Heyson (page images at HathiTrust)
• Langley Research Center: Monte Carlo analysis of inaccuracies in estimated aircraft parameters caused by unmodeled flight instrumentation errors (National Aeronautics and Space Administration ;, 1975), also by Ward F. Hodge and Wayne H. Bryant (page images at HathiTrust)
• Langley Research Center: A Monte Carlo analysis of the Viking lander dynamics at touchdown (National Aeronautics and Space Administration ;, 1975), also by Ralph J. Muraca, C. Anderson King, and Janet W. Campbell (page images at HathiTrust)
• Langley Research Center: A Monte Carlo investigation of experimental data requirements for fitting polynomial functions (National Aeronautics and Space Administration ;, 1974), also by George C. Canavos (page images at HathiTrust)
• Langley Research Center: Motion and interaction of decaying trailing vortices in spanwise shear wind (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by C. H. Liu and L. Ting (page images at HathiTrust)
• Langley Research Center: A motion-constraint logic for moving-base simulators based on variable filter parameters (National Aeronautics and Space Administration ;, 1974), also by G. Kimball Miller (page images at HathiTrust)
• Langley Research Center: Motion software for a synergistic six-degree-of-freedom motion base (National Aeronautics and Space Administration ;, 1973), also by Russell V. Parrish, Dennis J. Martin, and James E. Dieudonne (page images at HathiTrust)
• Langley Research Center: Motorless flight research, 1972. (National Aeronautics and Space Administration; [for sale by the National Technical Information Service, Springfield, Va.], 1973), also by Workshop to Identify Priorities for Motorless Flight Research (1972 : Massachusetts Institute of Technology), James L. Nash-Webber, Massachusetts Institute of Technology, and International Symposium on the Technology and Science of Motorless Flight (1st : 1972 : Massachusetts Institute of Technology) (page images at HathiTrust)
• Langley Research Center: Moving-base visual simulation study of decoupled controls during approach and landing of a STOL transport aircraft (National Aeronautics and Space Administration ;, 1975), also by G. Kimball Miller and Perry L. Deal (page images at HathiTrust)
• Langley Research Center: Moving-cockpit simulator investigation of the minimum tolerable longitudinal maneuvering stability (National Aeronautics and Space Administration, 1959), also by B. Porter Brown and Harold I. Johnson (page images at HathiTrust)
• Langley Research Center: Moving-cockpit-simulator study of piloted entries into the earth's atmosphere for a capsule-type vehicle at parabolic velocity (National Aeronautics and Space Administration, 1963), also by John W. Young, L. E. Barker, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Francis J. Capone and E. Ann Bare (page images at HathiTrust)
• Langley Research Center: Multidisciplinary optimization of controlled space structures with global sensitivity equations (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Sharon L. Padula (page images at HathiTrust)
• Langley Research Center: Multigrid methods for flow transition in three-dimensional boundary layers with surface roughness (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), also by Chaoqun Liu, Steve McCormick, Zhining Liu, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: Multilevel decomposition approach to the preliminary sizing of a transport aircraft wing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division :, 1990), also by Gregory A. Wrenn, Augustine R. Dovi, and Lockheed Engineering & Sciences Company (page images at HathiTrust)
• Langley Research Center: Multiple lesion track structure model (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by John W. Wilson, Judy L. Shinn, and Francis A. Cucinotta (page images at HathiTrust)
• Langley Research Center: Multiple-scale turbulence modeling of boundary layer flows for scramjet applications (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1981), also by G. Fabris, R. B. Edelman, P. T. Harsha, inc. Combustion Science and Advanced Technology Dept Science Applications, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Multiscale modeling, simulation and visualization and their potential for future aerospace systems : proceedings of the workshop sponsored by the National Aeronautics and Space Administration and Old Dominion University, Center for Advanced Engineering Environments, Hampton, Virginia : and held at NASA Langley Research Center, Hampton, Virginia, March 5-6, 2002 (National Aeronautics and Space Administration, Langley Research Center, 2002), also by Ahmed Khairy Noor and Old Dominion University. Center for Advanced Engineering Environments (page images at HathiTrust)
• Langley Research Center: Multiscale turbulence effects in supersonic jets exhausting into still air (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Khaled S. Abdol-Hamid and Richard G. Wilmoth (page images at HathiTrust)
• Langley Research Center: The multistate impact parameter method for molecular charge exchange in nitrogen (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Juliette W. Ioup and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Nacelle/pylon/wing integration on a transport model with a natural laminar flow nacelle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Milton Lamb, James C. Patterson, and William Kelly Abeyounis (page images at HathiTrust)
• Langley Research Center: Nanobiotechnology : proceedings of a workshop sponsored by the National Aeronautics and Space Administration and the University of Virginia Center for Advanced Computational Technology, Hampton, Virginia, and held at NASA Langley Research Center, Hampton, Virginia, June 14-15, 2000 (Langley Research Center, 2000), also by Ahmed Khairy Noor (page images at HathiTrust)
• Langley Research Center: The NASA Aircraft Noise Prediction Program improved Propeller Analysis System (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by L. Cathy Nguyen and Lockheed Engineering & Sciences Company (page images at HathiTrust)
• Langley Research Center: NASA conference on large space antenna systems technology, 1984 : December 4-6, 1984. (National Aeronautics and Space Administration, Langley Research Center, 1984), also by NASA Conference on Large Space Antenna Systems Technology (1984 : Langley Research Center) (page images at HathiTrust)
• Langley Research Center: NASA CR-1412 (National Aeronautics and Space Administration ;, 1969), also by C. B. Grosch, H. R. Paetznick, United States National Aeronautics and Space Administration, and Control Data Corporation (page images at HathiTrust)
• Langley Research Center: NASA CR-1440 (National Aeronautics and Space Administration ;, 1969), also by Anton J. Landgrebe, United Aircraft Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA CR-1441 (National Aeronautics and Space Administration ;, 1969), also by Anton J. Landgrebe, United Aircraft Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA CR-1577 (National Aeronautics and Space Administration ;, 1970), also by Vincent James Piarulli, Richard P. White, United States National Aeronautics and Space Administration, and Rochester Applied Sciences Associates (page images at HathiTrust)
• Langley Research Center: NASA CR-1789 (National Aeronautics and Space Administration ;, 1972), also by B. J. Kuchta, George R. Friedman, United States National Aeronautics and Space Administration, and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Langley Research Center: NASA CR-1983 (National Aeronautics and Space Administration, 1968), also by John W. Leverton, University of Southampton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA CR-2277 (National Aeronautics and Space Administration ;, 1973), also by R. M. Wright, AiResearch Manufacturing Company of Los Angeles (Calif.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA CR-2374 (National Aeronautics and Space Administration ;, 1974), also by David L. Kleinman, William R. Killingsworth, inc Systems Control, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA CR-327 (National Aeronautics and Space Administration ;, 1965), also by John C. Houbolt, Aeronautical Research Associates of Princeton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA High-speed Research Program Sonic Boom Workshop (National Aeronautics and Space Administration, Langley Research Center, 1996), also by Va.) High Speed Research Program Sonic Boom Workshop 1995 : Hampton and Daniel G. Baize (page images at HathiTrust)
• Langley Research Center: NASA Langley Formal Methods Workshop (National Aeronautics and Space Administration, Langley Research Center, 2000), also by Virginia) NASA Formal Methods Workshop (5th : 2000 : Williamsburg and C. Michael Holloway (page images at HathiTrust; US access only)
• Langley Research Center: The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : design overview (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Charles D. Harris, Cuyler W. Brooks, and William D. Harvey (page images at HathiTrust)
• Langley Research Center: The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : evaluation of initial perforated configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Charles D. Harris (page images at HathiTrust)
• Langley Research Center: The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : suction coefficient analysis (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Cuyler W. Brooks, William D. Harvey, and Charles D. Harris (page images at HathiTrust)
• Langley Research Center: NASA Langley ninety years on the leading edge since 1917 (National Aeronautics and Space Administration, Langley Research Center, 2007) (page images at HathiTrust)
• Langley Research Center: NASA participation in the 1980 persistent elevated pollution episode/northeast regional oxidant study (PEPE/NEROS) project : operational aspects (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by G. L. Maddrea, Richard J. Bendura, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: NASA progress in aircraft noise prediction (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by J. P. Raney, W. E. Zorumski, S. L. Padula, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: NASA supercritical airfoils : a matrix of family-related airfoils (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Charles D. Harris (page images at HathiTrust)
• Langley Research Center: NASA TLA workload analysis support (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by James L. Sundstrom and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: NASA TM X-1140 (National Aeronautics and Space Administration ;, 1965), also by Herbert D. Hendricks, Larry B. York, Thomas G. James, United States National Aeronautics and Space Administration, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Langley Research Center: NASA TM X-3470 (National Aeronautics and Space Administration :, 1977), also by Louis G. Kaufman, Charles B. Johnson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1248 (National Aeronautics and Space Administration ;, 1962), also by John E. Duberg and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1269 (National Aeronautics and Space Administration ;, 1962), also by John L. McCarty, Huey D. Carden, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1600 (National Aeronautics and Space Administration, 1963), also by John G. Presnell, R. L. McKinney, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1604 (National Aeronautics and Space Administration, 1963), also by Alton P. Mayo, Margery E. Hannah, Harold A. Hamer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1605 (National Aeronautics and Space Administration, 1963), also by David J. Romeo, James R. Sterrett, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1607 (National Aeronautics and Space Administration, 1963), also by Jack A. White and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1611 (National Aeronautics and Space Administration, 1963), also by Jack Levine and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1613 (National Aeronautics and Space Administration, 1963), also by Gary P. Beasley and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1614 (National Aeronautics and Space Administration, 1963), also by Robert E. Shanks and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1615 (National Aeronautics and Space Administration, 1963), also by Robert W. Fralich and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1617 (National Aeronautics and Space Administration, 1963), also by Gene W. Sparrow and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1623 (National Aeronautics and Space Administration, 1963), also by David F. Thomas, John D. Bird, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1624 (National Aeronautics and Space Administration, 1963), also by Sandy M. Stubbs and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1627 (National Aeronautics and Space Administration, 1963), also by William Gracey and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1628 (National Aeronautics and Space Administration, 1963), also by P. Calvin Stainback and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1629 (National Aeronautics and Space Administration, 1963), also by Raymond D. Vogler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1631 (National Aeronautics and Space Administration, 1963), also by S. Katzoff and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1632 (National Aeronautics and Space Administration, 1963), also by Wayne D. Erickson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1633 (National Aeronautics and Space Administration, 1963), also by George W. Jones, Jerome T. Foughner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1636 (National Aeronautics and Space Administration, 1963), also by Clarence W. Matthews and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1638 (National Aeronautics and Space Administration, 1963), also by Patrick J. Johnston and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1775 (National Aeronautics and Space Administration, 1963), also by Joseph J. Janos, John R. Unangst, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1776 (National Aeronautics and Space Administration ;, 1963), also by Dewey E. Wornom, Robert T. Taylor, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1779 (National Aeronautics and Space Administration :, 1963), also by James H. Otis, Kenneth W. Goodson, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1780 (National Aeronautics and Space Administration ;, 1963), also by Robert H. Tolson and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1781 (National Aeronautics and Space Administration ;, 1963), also by David S. Shaw, C. Donald Babb, Dennis E. Fuller, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1782 (National Aeronautics and Space Administration ;, 1963), also by James J. Adams and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1783 (National Aeronautics and Space Administration ;, 1963), also by William D. Beasley, RRaymond L. Barger, J. D. Brooks, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1784 (National Aeronautics and Space Administration ;, 1963), also by Donald H. Humes and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1785 (National Aeronautics and Space Administration ;, 1963), also by Charles R. Manning, Dick M. Royster, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1786 (National Aeronautics and Space Administration ;, 1963), also by Clarence A. Brown and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1788 (National Aeronautics and Space Administration ;, 1963), also by Joseph M. Groen, Richard Rosecrans, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1789 (National Aeronautics and Space Administration ;, 1963), also by Nickolai Charczenko and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1790 (National Aeronautics and Space Administration ;, 1963), also by Paul F. Holloway, James C. Dunavant, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1792 (National Aeronautics and Space Administration ;, 1963), also by E. Carson Yates and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1793 (National Aeronautics and Space Administration, 1963), also by Theodore J. Goldberg, James G. Hondros, George C. Ashby, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1795 (National Aeronautics and Space Administration, 1963), also by John B. Peterson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1796 (National Aeronautics and Space Administration, 1964), also by William P. Henderson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1800 (National Aeronautics and Space Administration, 1963), also by David J. Romeo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1801 (National Aeronautics and Space Administration, 1963), also by Paul A. Hunter, Mary W. Fetner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1802 (National Aeronautics and Space Administration, 1963), also by Henry L. Kelley, Robert A. Champine, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1803 (National Aeronautics and Space Administration, 1963), also by C. Michael Hudson, Herbert F. Hardrath, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1807 (National Aeronautics and Space Administration, 1963), also by Samuel R. Bland, Robert M. Bennett, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1809 (National Aeronautics and Space Administration, 1963), also by Richard J. Re and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1815 (National Aeronautics and Space Administration, 1963), also by Kenneth P. Spreemann and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1818 (National Aeronautics and Space Administration, 1963), also by David A. Hilton, Harvey H. Hubbard, Emedio M. Bracalente, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1820 (National Aeronautics and Space Administration, 1963), also by Harold A. Hamer, Ward F. Hodge, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1822 (National Aeronautics and Space Administration, 1963), also by Robert E. Shanks and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1823 (National Aeronautics and Space Administration, 1963), also by Odell A. Morris and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1861 (National Aeronautics and Space Administration :, 1964), also by Gregory R. Wichorek, Bland A. Stein, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1865 (National Aeronautics and Space Administration :, 1965), also by David G. Stephens, Maurice A. Scavullo, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1867 (National Aeronautics and Space Administration :, 1964), also by Emma Jean Landrum and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-1961 (National Aeronautics and Space Administration, 1963), also by Albin O. Pearson and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1963 (National Aeronautics and Space Administration, 1963), also by Bernard Spencer, W. Pelham Phillips, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1965 (National Aeronautics and Space Administration, 1963), also by Robert H. Kirby and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1966 (National Aeronautics and Space Administration, 1963), also by E. Carson Yates, Annie G. Fox, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1968 (National Aeronautics and Space Administration, 1963), also by Domenic J. Maglieri, John F. Bryant, Virgil S. Ritchie, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-1969 (National Aeronautics and Space Administration, 1963), also by James J. Adams, Hugh P. Bergeron, W. E. Howell, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2011 (National Aeronautics and Space Administration, 1963), also by David N. Braski, George J. Heimerl, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2012 (National Aeronautics and Space Administration, 1963), also by William Gracey, Joseph W. Stickle, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2014 (National Aeronautics and Space Administration, 1963), also by Matthew M. Winston, Robert J. Huston, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2016 (National Aeronautics and Space Administration, 1963), also by James L. Williams, L. Keith Barker, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2017 (National Aeronautics and Space Administration, 1963), also by James L. Raper and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2019 (National Aeronautics and Space Administration, 1963), also by Frank L. Clark, Charles B. Johnson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2023 (National Aeronautics and Space Administration ;, 1963), also by Fred M. Smith, Pierce L. Lawing, Edwin F. Harrison, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2025 (National Aeronautics and Space Administration, 1963), also by Henry S. Freynik and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2029 (National Aeronautics and Space Administration, 1963), also by Howard S. Carter and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2030 (National Aeronautics and Space Administration, 1963), also by Paul G. Fournier and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2031 (National Aeronautics and Space Administration, 1963), also by Joseph L. Johnson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2033 (National Aeronautics and Space Administration, 1963), also by Bernard Spencer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2038 (National Aeronautics and Space Administration ;, 1963), also by Perry W. Hanson, Gilbert M. Levey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2045 (National Aeronautics and Space Administration, 1963), also by I. E. Figge and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2048 (National Aeronautics and Space Administration, 1963), also by K. R. Czarnecki, William J. Monta, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2049 (National Aeronautics and Space Administration, 1963), also by Jack A. White and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2051 (National Aeronautics and Space Administration, 1963), also by E. Carson Yates, Samuel R. Bland, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2165 (National Aeronautics and Space Administration :, 1964), also by Marvin B. Dow and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2201 (National Aeronautics and Space Administration :, 1964), also by J. Wayne Keyes and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2243 (National Aeronautics and Space Administration :, 1965), also by William D. Grantham, Sue B. Grafton, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2300 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington D.C. 20230], 1964), also by Wayne S. Slemp and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2331 (National Aeronautics and Space Administration :, 1964), also by C. M. Hudson and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2340 (National Aeronautics and Space Administration :, 1964), also by Earl A. Price, Robert L. Stallings, Paul W. Howard, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2352 (National Aeronautics and Space Administration :, 1964), also by Dennis E. Fuller, Roger H. Fournier, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2360 (National Aeronautics and Space Administration :, 1964), also by Robert C. Goetz and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2380 (National Aeronautics and Space Administration :, 1964), also by Raymond D. Vogler and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2456 (National Aeronautics and Space Administration, 1964), also by Martin Milton Mikulas and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2462 (National Aeronautics and Space Administration :, 1964), also by George E. Sweet, Matthew M. Winston, Julian L. Jenkins, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2471 (National Aeronautics and Space Administration :, 1964), also by W. Thomas Blackshear, Donald G. Eide, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2477 (National Aeronautics and Space Administration :, 1964), also by John F. Garren, John P. Reeder, James R. Kelly, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2478 (National Aeronautics and Space Administration :, 1964), also by George F. Klich, Edward W. Leyhe, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2482 (National Aeronautics and Space Administration :, 1964), also by David L. Block and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2483 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), also by Lawrence W. Brown and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2486 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), also by Dewey E. Wornom, Joseph Gera, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2489 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), also by James P. Arrington, Arthur Henderson, Roy C. Joiner, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2492 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1965), also by Joseph L. Johnson and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2493 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), also by John D. Buckley, Bennie W. Cocke, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2497 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1965), also by William C. Thompson and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2499 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), also by David N. Braski and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-2616 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1965), also by Dick M. Royster, Cynthia A. Dysleski, Charles R. Manning, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-2783 (National Aeronautics and Space Administration :, 1965), also by Robert E. Fulton and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3066 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), also by Robert Miserentino, Louis F. Vosteen, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3075 (National Aeronautics and Space Administration :, 1965), also by Edward P. Phillips and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3152 (National Aeronautics and Space Administration :, 1965), also by John H. Crews and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3213 (National Aeronautics and Space Administration ;, 1966), also by Raymond D. Vogler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3216 (National Aeronautics and Space Administration ;, 1966), also by James A. Blackwell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3217 (National Aeronautics and Space Administration ;, 1966), also by Kenneth W. Goodson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3268 (National Aeronautics and Space Administration :, 1966), also by John R. McGhee and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3276 (National Aeronautics and Space Administration :, 1966), also by William J. Small, Mitchel H. Bertram, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3310 (National Aeronautics and Space Administration :, 1966), also by Robert L. Wright and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3390 (National Aeronautics and Space Administration :, 1966), also by Mark R. Nichols and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3466 (National Aeronautics and Space Administration ;, 1966), also by W. B. Fichter and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-3583 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 2215], 1966), also by William B. Kemp, W. Pelham Phillips, Vernard E. Lockwood, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3588 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 2215], 1966), also by John B. Peterson, William J. Monta, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3589 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 2215], 1966), also by K. R. Czarnecki and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3591 (National Aeronautics and Space Administration ;, 1966), also by Joseph R. Chambers, Sue B. Grafton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3600 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 2215], 1966), also by Robert J. Tapscott, Robert W. Sommer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3631 (National Aeronautics and Space Administration :, 1966), also by Paul E. Tippens, John R. Davidson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3661 (National Aeronautics and Space Administration :, 1966), also by Stanley H. Scher, Irene G. Young, James C. Dunavant, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-3735 (National Aeronautics and Space Administration [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia], 1966), also by Stephen S. Tompkins, Marvin B. Dow, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3737 (National Aeronautics and Space Administration ;, 1966), also by G. K. Oertel and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3738 (National Aeronautics and Space Administration ;, 1966), also by Harry H. Heyson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3871 (National Aeronautics and Space Administration :, 1967), also by James C. Dunavant, Howard W. Stone, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3891 (National Aeronautics and Space Administration :, 1967), also by Grayson V. Dixon, Jerome Pearson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3908 (National Aeronautics and Space Administration ;, 1967), also by Robert T. Swann, Ronald K. Clark, William D. Brewer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3916 (National Aeronautics and Space Administration ;, 1967), also by Richard Madden and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3918 (National Aeronautics and Space Administration ;, 1967), also by John G. Davis, George W. Zender, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3920 (National Aeronautics and Space Administration ;, 1967), also by Leonard V. Clark and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3929 (National Aeronautics and Space Administration ;, 1967), also by Jimmy M. Cawthorn, Clyde Hayes, Garland J. Morris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3932 (National Aeronautics and Space Administration ;, 1967), also by Vernard E. Lockwood and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3934 (National Aeronautics and Space Administration ;, 1967), also by Donald E. Hewes and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3969 (National Aeronautics and Space Administration ;, 1967), also by Luther Neal, Mitchel H. Bertram, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3970 (National Aeronautics and Space Administration ;, 1967), also by Norman R. Driscoll and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3972 (National Aeronautics and Space Administration ;, 1967), also by Howard G. Hatch, Jere B. Cobb, Jack E. Pennington, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3973 (National Aeronautics and Space Administration ;, 1967), also by John Locke McCarty, Jerome Pearson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3980 (National Aeronautics and Space Administration ;, 1967), also by Sandy M. Stubbs and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3986 (National Aeronautics and Space Administration ;, 1967), also by William Gracey, Don F. Tibbs, Robert W. Sommer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-3989 (National Aeronautics and Space Administration ;, 1967), also by J. B. Robertson, T. E. Gilmer, R. K. Franks, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4010 (National Aeronautics and Space Administration ;, 1967), also by Frank M. Bugg, William C. Sleeman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4011 (National Aeronautics and Space Administration ;, 1967), also by John T. Suttles, Lucille C. Coltrane, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4013 (National Aeronautics and Space Administration ;, 1967), also by James C. Ferris and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4014 (National Aeronautics and Space Administration ;, 1967), also by C. Donald Babb, Dennis E. Fuller, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4021 (National Aeronautics and Space Administration ;, 1967), also by Donald L. Loving, Arvo A. Luoma, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4028 (National Aeronautics and Space Administration ;, 1967), also by Fred R. DeJarnette and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4030 (National Aeronautics and Space Administration ;, 1967), also by Marvin P. Fink and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4034 (National Aeronautics and Space Administration ;, 1967), also by Lawrence E. Putnam and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4044 (National Aeronautics and Space Administration ;, 1967), also by John A. Zalovcik, William T. Schaefer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4061 (National Aeronautics and Space Administration ;, 1967), also by L.A. Imig and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4062 (National Aeronautics and Space Administration ;, 1967), also by Marvin P. Fink and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4063 (National Aeronautics and Space Administration ;, 1967), also by W. Wayne Scott and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4064 (National Aeronautics and Space Administration ;, 1967), also by William F. Hinson, Robert J. McGhee, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4073 (National Aeronautics and Space Administration ;, 1967), also by James P. Peterson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4077 (National Aeronautics and Space Administration ;, 1967), also by Ernie L. Anglin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4079 (National Aeronautics and Space Administration ;, 1967), also by Bernard Spencer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4080 (National Aeronautics and Space Administration ;, 1967), also by James Wayne Sawyer, William D. Deveikis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4083 (National Aeronautics and Space Administration ;, 1967), also by Raymond D. Vogler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4084 (National Aeronautics and Space Administration ;, 1967), also by Kenneth P. Spreemann and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4085 (National Aeronautics and Space Administration ;, 1967), also by Milton D. McLaughlin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4089 (National Aeronautics and Space Administration ;, 1967), also by G. Kimball Miller, L. Keith Barker, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4090 (National Aeronautics and Space Administration ;, 1967), also by David A. Evensen and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4120 (National Aeronautics and Space Administration ;, 1967), also by Daniel J. DiCarlo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4170 (National Aeronautics and Space Administration ;, 1967), also by Richard H. Sawyer, Norman S. Silsby, Milton D. McLaughlin, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4229 (National Aeronautics and Space Administration ;, 1967), also by Thomas R. Turner and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4241 (National Aeronautics and Space Administration ;, 1967), also by John A. Zalovcik and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4357 (National Aeronautics and Space Administration ;, 1968), also by Robert W. Fralich, John A. McElman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4358 (National Aeronautics and Space Administration ;, 1968), also by I. E. Figge and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4361 (National Aeronautics and Space Administration ;, 1968), also by David R. Stone, George C. Ashby, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4367 (National Aeronautics and Space Administration ;, 1968), also by Davis H. Crawford and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4372 (National Aeronautics and Space Administration ;, 1968), also by Nancy Jane Cyrus, Robert E. Fulton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4401 (National Aeronautics and Space Administration ;, 1968), also by K. R. Czarnecki, Russell B. Sorrells, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4425 (National Aeronautics and Space Administration ;, 1968), also by W. Jefferson Stroud, Nancy P. Sykes, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4427 (National Aeronautics and Space Administration ;, 1968), also by John E. Lamar and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4434 (National Aeronautics and Space Administration ;, 1968), also by James T. Howlett and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4436 (National Aeronautics and Space Administration ;, 1968), also by Cuyler W. Brooks and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4443 (National Aeronautics and Space Administration ;, 1968), also by Dennis M. Bushnell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4454 (National Aeronautics and Space Administration ;, 1968), also by John L. McCarty, Huey D. Carden, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4466 (National Aeronautics and Space Administration ;, 1968), also by K. W. Böer, E. J. Conway, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4471 (National Aeronautics and Space Administration ;, 1968), also by W. J. Tuovila, Norman S. Land, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4474 (National Aeronautics and Space Administration ;, 1968), also by Ulysse J. Blanchard and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4484 (National Aeronautics and Space Administration ;, 1968), also by Ernest V. Zoby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4494 (National Aeronautics and Space Administration ;, 1968), also by W. Douglas Morris, Lana M. Couch, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4501 (National Aeronautics and Space Administration ;, 1968), also by Friedrich O. Huck and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4502 (National Aeronautics and Space Administration ;, 1968), also by James A. Schoenster, Robert R. Clary, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4524 (National Aeronautics and Space Administration ;, 1968), also by John J. Broderick and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4528 (National Aeronautics and Space Administration ;, 1968), also by Jag J. Singh, Emanuel Rind, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4532 (National Aeronautics and Space Administration ;, 1968), also by John M. Jerke, Atwood R. Heath, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4543 (National Aeronautics and Space Administration ;, 1968), also by Dennis M. Bushnell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4555 (National Aeronautics and Space Administration ;, 1968), also by C. R. Cockrell, W. F. Croswell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4556 (National Aeronautics and Space Administration ;, 1968), also by Hans-Juergen C. Blume and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4563 (National Aeronautics and Space Administration ;, 1968), also by Jerry C. South and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4574 (National Aeronautics and Space Administration ;, 1968), also by William J. Snyder and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4598 (National Aeronautics and Space Administration ;, 1968), also by George C. Ashby, W. Frank Staylor, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4602 (National Aeronautics and Space Administration ;, 1968), also by Thomas A. Byrdsong and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4655 (National Aeronautics and Space Administration ;, 1968), also by Robert V. Doggett, A. Gerald Rainey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4664 (National Aeronautics and Space Administration ;, 1968), also by Joseph W. Stickle, Robert C. Henry, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4671 (National Aeronautics and Space Administration ;, 1968), also by William D. Harvey and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4672 (National Aeronautics and Space Administration ;, 1968), also by George M. Ware, Charles E. Libbey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4680 (National Aeronautics and Space Administration ;, 1968), also by Robert W. Herr and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4681 (National Aeronautics and Space Administration ;, 1968), also by William S. Lassiter and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-4685 (National Aeronautics and Space Administration ;, 1968), also by Casimir J. Jachimowski, William M. Houghton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4713 (National Aeronautics and Space Administration ;, 1968), also by Randolph A. Graves, William G. Witte, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4719 (National Aeronautics and Space Administration ;, 1968), also by James F. Campbell, Dorothy T. Howell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4720 (National Aeronautics and Space Administration ;, 1968), also by Fred R. DeJarnette, Ruby M. Davis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4726 (National Aeronautics and Space Administration ;, 1968), also by Delma C. Freeman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4737 (National Aeronautics and Space Administration ;, 1968), also by Floyd G. Howard and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4739 (National Aeronautics and Space Administration ;, 1968), also by Edward C. Polhamus and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4740 (National Aeronautics and Space Administration ;, 1968), also by T.M. Walsh, Dwayne E. Hinton, Jean C. Keating, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4742 (National Aeronautics and Space Administration ;, 1968), also by T. M. Walsh and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4746 (National Aeronautics and Space Administration :, 1968), also by William J. Monta, William D. Deveikis, K. R. Czarnecki, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4750 (National Aeronautics and Space Administration ;, 1968), also by Kenneth Sutton and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4791 (National Aeronautics and Space Administration :, 1968), also by Thomas E. Walton, Brian J. O'Hare, William G. Witte, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4842 (National Aeronautics and Space Administration :, 1968), also by James J. Adams, Hugh P. Bergeron, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-4871 (National Aeronautics and Space Administration :, 1968), also by Howard M. Adelman, Earl C. Steeves, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-4889 (National Aeronautics and Space Administration ;, 1968), also by Marvin D. Rhodes, Conrad M. Willis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4891 (National Aeronautics and Space Administration :, 1969), also by Charles H. Fox and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-4892 (National Aeronautics and Space Administration ;, 1968), also by John C. Hoppe and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4900 (National Aeronautics and Space Administration ;, 1968), also by John W. Wilson, George G. Steinmetz, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4901 (National Aeronautics and Space Administration ;, 1968), also by Herbert D. Hendricks, Donald H. Phillips, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4906 (National Aeronautics and Space Administration ;, 1968), also by Clarence D. Cone, Kathryn H. Peddrew, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4907 (National Aeronautics and Space Administration :, 1968), also by James P. Arrington and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4914 (National Aeronautics and Space Administration :, 1968), also by G. Burton Northam and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-4961 (National Aeronautics and Space Administration ;, 1969), also by P. Calvin Stainback and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5031 (National Aeronautics and Space Administration ;, 1968), also by Thomas G. Gainer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5045 (National Aeronautics and Space Administration :, 1968), also by John D. Bird and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5046 (National Aeronautics and Space Administration ;, 1969), also by Charlie M. Jackson, Rudeen S. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5121 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by James C. Ellison and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5160 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Howard W. Stone and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5199 (National Aeronautics and Space Administration ;, 1969), also by George M. Ware and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5200 (National Aeronautics and Space Administration ;, 1969), also by Frank Hohl and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5201 (National Aeronautics and Space Administration ;, 1969), also by Robert J. McGhee, W. Frank Staylor, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5202 (National Aeronautics and Space Administration ;, 1969), also by Jack D. Leatherwood, David G. Stephens, Grayson V. Dixon, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5204 (National Aeronautics and Space Administration ;, 1969), also by James F. Campbell, Dorothy H. Tudor, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5219 (National Aeronautics and Space Administration ;, 1969), also by Edwin E. Davenport and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5230 (National Aeronautics and Space Administration ;, 1969), also by George E. Sweet and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5233 (National Aeronautics and Space Administration ;, 1969), also by Robert C. Goetz and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5235 (National Aeronautics and Space Administration ;, 1969), also by Otto F. Trout, Donald L. Jacobs, Gary P. Beasley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5236 (National Aeronautics and Space Administration ;, 1969), also by John R. McGehee, Cornelia B. Dexter, Melvin E. Hathaway, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5251 (National Aeronautics and Space Administration ;, 1969), also by James L. Hunt and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5254 (National Aeronautics and Space Administration ;, 1969), also by Donald R. Rummler, Gregory R. Wichorek, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5256 (National Aeronautics and Space Administration ;, 1969), also by Robert J. Huston, James P. Shivers, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5270 (National Aeronautics and Space Administration :, 1969), also by Robert J. Pegg and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5278 (National Aeronautics and Space Administration ;, 1969), also by L. Roane Hunt, R. R. Howell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5295 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by William L. Wells and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5297 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Lana M. Couch and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5306 (National Aeronautics and Space Administration ;, 1969), also by William D. Beasley, Raymond L. Barger, J. D. Brooks, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5307 (National Aeronautics and Space Administration ;, 1969), also by Russell B. Sorrells, Lorraine F. Satchell, K. R. Czarnecki, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5308 (National Aeronautics and Space Administration ;, 1969), also by Alphonsa Smith and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5314 (National Aeronautics and Space Administration ;, 1969), also by Francis J. Capone, Harry T. Norton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5315 (National Aeronautics and Space Administration ;, 1969), also by James M. Eggers, Marvin G. Torrence, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5316 (National Aeronautics and Space Administration ;, 1969), also by Francis J. Capone and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5334 (National Aeronautics and Space Administration ;, 1969), also by James F. Campbell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5335 (National Aeronautics and Space Administration ;, 1969), also by James A. Blackwell and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5342 (National Aeronautics and Space Administration :, 1969), also by Frank R. Niessen and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5361 (National Aeronautics and Space Administration ;, 1969), also by Joseph R. Chambers, Ernie L. Anglin, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5362 (National Aeronautics and Space Administration ;, 1969), also by Edward P. Phillips and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5365 (National Aeronautics and Space Administration ;, 1969), also by James F. Campbell, Josephine W. Grow, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5379 (National Aeronautics and Space Administration ;, 1969), also by John P. Decker and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5392 (National Aeronautics and Space Administration ;, 1969), also by Robert L. Stallings, Dorothy T. Howell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5393 (National Aeronautics and Space Administration ;, 1969), also by Bobbly Lee Berrier, Frederick H. Wood, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5397 (National Aeronautics and Space Administration ;, 1969), also by G. Burton Northam, Wayne P. Jessee, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5408 (National Aeronautics and Space Administration ;, 1969), also by Delma C. Freeman, Richard D'Amato, Sue B. Grafton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5409 (National Aeronautics and Space Administration :, 1969), also by Joseph R. Chambers, Ernie L. Anglin, James S. Bowman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5410 (National Aeronautics and Space Administration ;, 1969), also by John F. Ward and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5418 (National Aeronautics and Space Administration ;, 1969), also by J. Wayne Keyes and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5419 (National Aeronautics and Space Administration ;, 1969), also by Alfredo Navarro Crespo, Herbert J. Cunningham, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5432 (National Aeronautics and Space Administration :, 1970), also by Paul Kuhn and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5433 (National Aeronautics and Space Administration ;, 1969), also by Dennis M. Bushnell, William V. Feller, William D. Harvey, Charles B. Johnson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5434 (National Aeronautics and Space Administration ;, 1969), also by L. Bernard Garrett, John N. Perkins, John T. Suttles, North Carolina State University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5438 (National Aeronautics and Space Administration ;, 1969), also by Waldo I. Oehman, Sylvia A. Wallace, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5454 (National Aeronautics and Space Administration ;, 1969), also by Allen H. Whitehead and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5466 (National Aeronautics and Space Administration :, 1970), also by William D. Grantham, James M. Patton, Perry L. Deal, Frederikc L. Moore, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5481 (National Aeronautics and Space Administration ;, 1969), also by Marvin P. Fink, Charles C. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5494 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by William D. Stanley, Doris M. Higgins, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5496 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by William D. Harvey, Ivan E. Beckwith, Dennis M. Bushnell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5498 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Theodore J. Goldberg, David R. Stone, Jerry N. Hefner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5499 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by James F. Campbell, Dorothy T. Howell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5508 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Charles P. Shore and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5524 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Gregory R. Wichorek, Bland A. Stein, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5525 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Richard E. Turner and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5535 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Melvin S. Anderson, Martin M. Mikulas, Herman L. Bohon, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5536 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Richard W. Faison, William H. Richards, John L. Gilbert, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5537 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Vincent R. Mascitti and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5538 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Irving Abel and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5553 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Lawrence E. Putnam, Francis J. Capone, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5555 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Herman L. Bohon, Walter L. Heard, Melvin S. Anderson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5556 (National Aeronautics and Space Administration :, 1969), also by Deene J. Weidman and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5561 (National Aeronautics and Space Administration :, 1969), also by James P. Peterson and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5581 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by H. Clyde McLemore, Patricia G. Hemeter, Charles C. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5600 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by Lloyd S. Jernell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5602 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by Julian L. Jenkins, Perry L. Deal, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5636 (National Aeronautics and Space Administration :, 1970), also by James Wayne Sawyer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5655 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by Charles E. Mercer, Bobby L. Berrier, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5660 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by Jerry M. Allen and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5661 (National Aeronautics and Space Administration :, 1970), also by John E. Lamar and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5662 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by Arthur W. Carter and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5663 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by John L. Sewall, Donnell S. Catherines, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5664 (National Aeronautics and Space Administration :, 1970), also by Harry G. Schaeffer and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5696 (National Aeronautics and Space Administration ;, 1970), also by George F. Sykes and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5697 (National Aeronautics and Space Administration :, 1970), also by John G. Davis and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5698 (National Aeronautics and Space Administration :, 1970), also by John Locke McCarty and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5699 (National Aeronautics and Space Administration :, 1970), also by Walter Brooks Drew and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5701 (National Aeronautics and Space Administration ;, 1970), also by George E. Weeks, Joseph E. Waltz, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5702 (National Aeronautics and Space Administration :, 1970), also by C. M. Hudson, K. N. Raju, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5712 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by Windsor L. Sherman and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5723 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by Willard E. Meador and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5724 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by William E. Miller and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5725 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by Willard W. Anderson, Kenneth L. Jacobs, Ralph W. Will, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5726 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by William F. White, Wesley C. Easley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5750 (National Aeronautics and Space Administration :, 1970), also by Robert Miserentino, Herman L. Bohon, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5753 (National Aeronautics and Space Administration ;, 1969), also by Charles B. Johnson, Dennis M. Bushnell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5754 (National Aeronautics and Space Administration, 1970), also by W. Frank Staylor and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5759 (National Aeronautics and Space Administration :, 1970), also by Sidney C. Dixon, M. Latrelle Hudson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5766 (National Aeronautics and Space Administration :, 1970), also by Michael C. Fischer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5767 (National Aeronautics and Space Administration :, 1970), also by Albert W. Hall and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5768 (National Aeronautics and Space Administration :, 1970), also by Wayne D. Erickson, George F. Klich, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5769 (National Aeronautics and Space Administration ;, 1970), also by Stephen S. Tompkins and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5777 (National Aeronautics and Space Administration :, 1970), also by R. A. Outlaw and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5779 (National Aeronautics and Space Administration :, 1970), also by Jay C. Hardin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5791 (National Aeronautics and Space Administration :, 1970), also by John Benjamin Anders and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5792 (National Aeronautics and Space Administration ;, 1970), also by Walter B. Olstad and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5793 (National Aeronautics and Space Administration :, 1970), also by Harry L. Morgan and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5801 (National Aeronautics and Space Administration ;, 1970), also by Robert K. Sleeper, Harold C. Lester, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5803 (National Aeronautics and Space Administration ;, 1970), also by Larry D. Pinson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5804 (National Aeronautics and Space Administration :, 1970), also by George F. Sykes and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5805 (National Aeronautics and Space Administration :, 1970), also by Edward J. Ray, Robert T. Taylor, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5816 (National Aeronautics and Space Administration :, 1970), also by William D. Deveikis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5817 (National Aeronautics and Space Administration :, 1970), also by George J. Hurt, James J. Adams, Hugh P. Bergeron, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5819 (National Aeronautics and Space Administration :, 1970), also by Harry H. Heyson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5831 (National Aeronautics and Space Administration :, 1970), also by Sumner A. Leadbetter and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5856 (National Aeronautics and Space Administration :, 1970), also by James P. Peterson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5857 (National Aeronautics and Space Administration ;, 1970), also by James P. Shivers, George M. Ware, Marvin P. Fink, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5859 (National Aeronautics and Space Administration :, 1970), also by John M. Jerke, Atwood R. Heath, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5861 (National Aeronautics and Space Administration :, 1970), also by William F. Hinson, Dennis M. Bushnell, Paul B. Gooderum, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5862 (National Aeronautics and Space Administration :, 1970), also by William D. Grantham, Robert W. Sommer, Perry L. Deal, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5863 (National Aeronautics and Space Administration :, 1970), also by Aubrey M. Cary and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5864 (National Aeronautics and Space Administration ;, 1970), also by Otto F. Trout and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5881 (National Aeronautics and Space Administration :, 1970), also by Eugene L. Kelsey, H. Milton Holt, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5882 (National Aeronautics and Space Administration :, 1970), also by Willard E. Meador and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5883 (National Aeronautics and Space Administration :, 1970), also by Willard E. Meador and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5884 (National Aeronautics and Space Administration :, 1970), also by C. W. Chiang, Richard D. Wagner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5885 (National Aeronautics and Space Administration :, 1970), also by William J. Small, David E. Fetterman, Frank S. Kirkham, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5893 (National Aeronautics and Space Administration ;, 1970), also by Rodger L. Naeseth and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5895 (National Aeronautics and Space Administration :, 1970), also by Leonard V. Clark and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5896 (National Aeronautics and Space Administration :, 1970), also by Alton P. Mayo and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5897 (National Aeronautics and Space Administration :, 1970), also by Robert S. Dunning and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5898 (National Aeronautics and Space Administration :, 1970), also by James C. Townsend and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5899 (National Aeronautics and Space Administration :, 1970), also by Charles B. Johnson and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5900 (National Aeronautics and Space Administration :, 1970), also by Blair B. Gloss and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5901 (National Aeronautics and Space Administration :, 1970), also by Charles G. Miller and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5907 (National Aeronautics and Space Administration :, 1970), also by Ralph A. Falanga, Edward M. Sullivan, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5908 (National Aeronautics and Space Administration :, 1970), also by Allan R. Wieting and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5909 (National Aeronautics and Space Administration :, 1970), also by Willard E. Meador and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5910 (National Aeronautics and Space Administration :, 1970), also by Doyle P. Swofford and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5911 (National Aeronautics and Space Administration ;, 1970), also by Harry L. Morgan, Charles F. Bradshaw, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5921 (National Aeronautics and Space Administration :, 1970), also by Joseph R. Chambers, James S. Bowman, Ernie L. Anglin, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5922 (National Aeronautics and Space Administration :, 1970), also by Sanger M. Burk and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5929 (National Aeronautics and Space Administration :, 1970), also by Ruben L. Jones and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5930 (National Aeronautics and Space Administration :, 1970), also by Kenneth Sutton and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5931 (National Aeronautics and Space Administration :, 1970), also by Jerry W. Deaton and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5937 (National Aeronautics and Space Administration ;, 1970), also by Leonard M. Weinstein and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5938 (National Aeronautics and Space Administration :, 1970), also by H. Benson Dexter and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5939 (National Aeronautics and Space Administration :, 1970), also by Williard W. Anderson, Ralph W. Will, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5940 (National Aeronautics and Space Administration :, 1970), also by G. Kimball Miller and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5941 (National Aeronautics and Space Administration :, 1970), also by John F. Newcomb, William F. Hampshire, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5942 (National Aeronautics and Space Administration ;, 1970), also by William A. Newsom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5943 (National Aeronautics and Space Administration :, 1970), also by Robert R. Clary, Lloyd J. Turner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5944 (National Aeronautics and Space Administration :, 1970), also by Felix L. Pitts, J. Larry Spencer, and National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5946 (National Aeronautics and Space Administration :, 1970), also by Jag J. Singh and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5947 (National Aeronautics and Space Administration :, 1970), also by W. B. Fichter and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5948 (National Aeronautics and Space Administration :, 1970), also by Gerard E. Woodbury, W. Douglas Morris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5965 (National Aeronautics and Space Administration :, 1970), also by Paul G. Fournier and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5971 (National Aeronautics and Space Administration :, 1970), also by Francis J. Capone and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5973 (National Aeronautics and Space Administration :, 1970), also by L. A. Imig and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5974 (National Aeronautics and Space Administration :, 1970), also by Paul G. Fournier, William C. Sleeman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5975 (National Aeronautics and Space Administration :, 1970), also by Chase P. Hearn and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5978 (National Aeronautics and Space Administration :, 1970), also by C. R. Cockrell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5979 (National Aeronautics and Space Administration :, 1970), also by Edmund J. Conway and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5980 (National Aeronautics and Space Administration :, 1970), also by Sidney C. Dixon, John B. Carine, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5981 (National Aeronautics and Space Administration :, 1970), also by A. Gary Childs, Athena T. Markos, Ernest S. Armstrong, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-5982 (National Aeronautics and Space Administration :, 1970), also by Milton D. McLaughlin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5986 (National Aeronautics and Space Administration :, 1970), also by Walter L. Heard, Herman L. Bohon, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5987 (National Aeronautics and Space Administration ;, 1970), also by Lawrence P. Shomo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-5988 (National Aeronautics and Space Administration:, 1970), also by Raymond D. Vogler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6003 (National Aeronautics and Space Administration :, 1970), also by Moses G. Farmer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6004 (National Aeronautics and Space Administration :, 1970), also by Allen G. McLain and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6005 (National Aeronautics and Space Administration :, 1970), also by Mervin E. Hillard, Richard W. Storey, Stewart L. Ocheltree, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6006 (National Aeronautics and Space Administration :, 1970), also by Sherman A. Clevenson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6017 (National Aeronautics and Space Administration :, 1970), also by Roger M. Winebarger and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6024 (National Aeronautics and Space Administration :, 1970), also by Gilbert A. Haynes and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6025 (National Aeronautics and Space Administration :, 1970), also by R. Earl Dunham, Robert W. Sommer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6031 (National Aeronautics and Space Administration :, 1970), also by Richard W. Barnwell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6059 (National Aeronautics and Space Administration ;, 1971), also by Wendell B. Stephens, Martha P. Robinson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6060 (National Aeronautics and Space Administration :, 1971), also by James M. Cubbage, F. S. Kirkham, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6061 (National Aeronautics and Space Administration :, 1971), also by Marvin G. Torrence and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6062 (National Aeronautics and Space Administration :, 1970), also by William L. Grantham and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6087 (National Aeronautics and Space Administration:, 1970), also by H. Wayne Leonard, William R. Cofer, Homer G. Morgan, Martin M. Mikulas, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6089 (National Aeronautics and Space Administration :, 1971), also by John L. Sewall, Christine G. Pusey, William M. Thompson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6090 (National Aeronautics and Space Administration :, 1971), also by James A. Schoenster and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6091 (National Aeronautics and Space Administration ;, 1971), also by Sue B. Grafton, Charles E. Libbey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6092 (National Aeronautics and Space Administration :, 1970), also by Willard E. Meador and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6100 (National Aeronautics and Space Administration :, 1971), also by Howard M. Adelman, Donnell S. Catherines, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6101 (National Aeronautics and Space Administration ;, 1970), also by James Scheiman, James P. Shivers, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6103 (National Aeronautics and Space Administration ;, 1971), also by James A. Martin, Robert J. McGhee, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6105 (National Aeronautics and Space Administration :, 1971), also by Cecil Eugene Kirby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6106 (National Aeronautics and Space Administration :, 1971), also by Robert Miserentino, Sidney C. Dixon, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6108 (National Aeronautics and Space Administration ;, 1971), also by John F. Garren and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6110 (National Aeronautics and Space Administration ;, 1971), also by Hugh P. Bergeron, George J. Hurt, James J. Adams, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6111 (National Aeronautics and Space Administration :, 1971), also by George J. Hurt, Marion A. Wise, David B. Middleton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6114 (National Aeronautics and Space Administration :, 1971), also by R. Clayton Rogers and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6116 (National Aeronautics and Space Administration :, 1970), also by Joseph H. Judd and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6117 (National Aeronautics and Space Administration ;, 1971), also by Frederick L. Moore and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6118 (National Aeronautics and Space Administration :, 1971), also by Robert J. Huston, Charles E. K. Morris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6119 (National Aeronautics and Space Administration :, 1971), also by Samuel Katzoff and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6121 (National Aeronautics and Space Administration ;, 1971), also by W. Jefferson Stroud and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6122 (National Aeronautics and Space Administration :, 1971), also by Willard E. Meador and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6123 (National Aeronautics and Space Administration ;, 1971), also by Griffin Y. Anderson, William Roger Russin, Anthony M. Agnone, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6124 (National Aeronautics and Space Administration :, 1971), also by Paul A. Hunter and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6126 (National Aeronautics and Space Administration :, 1971), also by L. Keith Barker, Gene W. Sparrow, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6127 (National Aeronautics and Space Administration :, 1971), also by Harry H. Heyson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6128 (National Aeronautics and Space Administration :, 1971), also by Philip C. Kassel, John D. DiBattista, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6130 (National Aeronautics and Space Administration ;, 1971), also by William E. Howell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6133 (National Aeronautics and Space Administration :, 1971), also by Paul A. Cooper, Martha P. Robinson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6134 (National Aeronautics and Space Administration :, 1971), also by Carl R. Pearson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6135 (National Aeronautics and Space Administration ;, 1971), also by Jerry G. Williams and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6138 (National Aeronautics and Space Administration :, 1971), also by James Campbell Robinson, George F. Klich, Robert R. McWithey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6140 (National Aeronautics and Space Administration ;, 1971), also by L. David Wall, Michael F. Card, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6142 (National Aeronautics and Space Administration ;, 1971), also by Richard J. Margason, John E. Lamar, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6144 (National Aeronautics and Space Administration ;, 1971), also by Clarence W. Matthews and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6192 (National Aeronautics and Space Administration ;, 1971), also by Ivan E. Beckwith, Frank L. Clark, William D. Harvey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6198 (National Aeronautics and Space Administration ;, 1971), also by William A. Newsom, Sue B. Grafton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6218 (National Aeronautics and Space Administration ;, 1971), also by Jarrell R. Elliott, William F. Teague, University of Kansas, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6220 (National Aeronautics and Space Administration ;, 1971), also by Stephen S. Tompkins and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6224 (National Aeronautics and Space Administration ;, 1971), also by George E. Sweet and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6239 (National Aeronautics and Space Administration ;, 1971), also by Robert J. Keynton and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6240 (National Aeronautics and Space Administration ;, 1971), also by Dennis O. Allison, Percy J. Bobbitt, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6242 (National Aeronautics and Space Administration ;, 1971), also by David C. Spence and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6257 (National Aeronautics and Space Administration ;, 1971), also by Jack D. Leatherwood and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6258 (National Aeronautics and Space Administration ;, 1971), also by James R. Williams, H. Andrew Wallio, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6265 (National Aeronautics and Space Administration ;, 1971), also by Elden S. Cornette, Edward M. Sullivan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6280 (National Aeronautics and Space Administration ;, 1971), also by Theodore J. Goldberg, Jerry N. Hefner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6281 (National Aeronautics and Space Administration ;, 1971), also by William D. Deveikis, James Wayne Sawyer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6282 (National Aeronautics and Space Administration ;, 1971), also by Bruce M. Kendall and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6292 (National Aeronautics and Space Administration ;, 1971), also by Kalman J. Grunwald and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6293 (National Aeronautics and Space Administration ;, 1971), also by William G. Witte and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6294 (National Aeronautics and Space Administration ;, 1971), also by Charles J. Schexnayder, John S. Evans, Paul W. Huber, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6298 (National Aeronautics and Space Administration ;, 1971), also by Gale A. Harvey and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6299 (National Aeronautics and Space Administration ;, 1971), also by David B. Middleton, George J. Hurt, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6300 (National Aeronautics and Space Administration ;, 1971), also by Earle K. Huckins, Lamont R. Poole, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6310 (National Aeronautics and Space Administration ;, 1971), also by Howard G. Maahs and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6340 (National Aeronautics and Space Administration ;, 1971), also by W. E. Zorumski and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6343 (National Aeronautics and Space Administration ;, 1971), also by Harold A. Hamer, Katherine G. Johnson, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6344 (National Aeronautics and Space Administration ;, 1971), also by Edwin E. Davenport, Jarrett K. Huffman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6346 (National Aeronautics and Space Administration ;, 1971), also by L. Keith Barker and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6374 (National Aeronautics and Space Administration :, 1971), also by John Q. Howell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6376 (National Aeronautics and Space Administration :, 1971), also by J. C. Newman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6416 (National Aeronautics and Space Administration ;, 1971), also by Harry H. Heyson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6423 (National Aeronautics and Space Administration ;, 1971), also by Stanley H. Scher, Irene G. Young, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6426 (National Aeronautics and Space Administration ;, 1971), also by John A. Tanner, Sidney A. Batterson, John L. McCarty, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6430 (National Aeronautics and Space Administration ;, 1971), also by Joseph Gera and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6445 (National Aeronautics and Space Administration ;, 1971), also by Daniel I. Sebacher, Louise P. Lee, Robert W. Guy, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6446 (National Aeronautics and Space Administration :, 1971), also by M. Schorling and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6447 (National Aeronautics and Space Administration :, 1971), also by Leonard R. McMaster and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6461 (National Aeronautics and Space Administration ;, 1971), also by Harold A. Hamer, Katherine G. Johnson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6462 (National Aeronautics and Space Administration :, 1971), also by Michael C. Fischer, Dal V. Maddalon, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6471 (National Aeronautics and Space Administration :, 1971), also by Robert J. Platt, Marvin D. Rhodes, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6473 (National Aeronautics and Space Administration ;, 1971), also by Eugene C. Naumann, William C. Walton, Donnell S. Catherines, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6478 (National Aeronautics and Space Administration :, 1971), also by Eugene L. Kelsey, Richard N. Young, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6479 (National Aeronautics and Space Administration :, 1971), also by Gary L. Giles and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6488 (National Aeronautics and Space Administration ;, 1971), also by David B. Middleton, George J. Hurt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6504 (National Aeronautics and Space Administration :, 1971), also by R. K. Franks, J. B. Robertson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6517 (National Aeronautics and Space Administration :, 1971), also by James A. Schoenster and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6546 (National Aeronautics and Space Administration ;, 1971), also by Donald J. Progar, William R. Wade, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6547 (National Aeronautics and Space Administration :, 1971), also by Arlen F. Carter and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6549 (National Aeronautics and Space Administration :, 1971), also by A. Gary Childs and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6557 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), also by Eugene C. Naumann, John S. Mixson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6570 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), also by Herbert A. Leybold and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6583 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), also by Ward F. Hodge and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6584 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), also by Bruce A. Conway and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6598 (National Aeronautics and Space Administration :, 1972), also by Richard N. Green, George R. Young, Lawrence H. Hoffman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6624 (National Aeronautics and Space Administration :, 1972), also by Howard G. Maahs and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6625 (National Aeronautics and Space Administration :, 1972), also by G. Burton Northam and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6626 (National Aeronautics and Space Administration :, 1972), also by John M. Jerke, Robert J. Platt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6629 (National Aeronautics and Space Administration :, 1972), also by William B. Kemp and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6631 (National Aeronautics and Space Administration :, 1972), also by Marvin E. Beatty and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6643 (National Aeronautics and Space Administration :, 1972), also by William T. Suit and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6656 (National Aeronautics and Space Administration :, 1972), also by Irving Abel and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6672 (National Aeronautics and Space Administration :, 1972), also by W. L. Snow and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6673 (National Aeronautics and Space Administration :, 1972), also by George G. Steinmetz, Jag J. Singh, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6677 (National Aeronautics and Space Administration :, 1972), also by Frederick C. Grant and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6709 (National Aeronautics and Space Administration :, 1972), also by Robert E. King, Gregory W. Condon, U.S. Army Air Mobility Research and Development Laboratory, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TN D-6710 (National Aeronautics and Space Administration :, 1972), also by Frederick W. Gibson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6711 (National Aeronautics and Space Administration :, 1972), also by Allen G. McLain, Warren C. Kelliher, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6733 (National Aeronautics and Space Administration :, 1972), also by L. Keith Barker, Gene W. Sparrow, Daniel J. Crawford, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-6759 (National Aeronautics and Space Administration ;, 1972), also by Jerry M. Allen and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-7002 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), also by Sherwood Hoffman, Joseph J. Janos, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-7066 (National Aeronautics and Space Administration ;, 1973), also by Perry W. Hanson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-7924 (National Aeronautics and Space Administration ;, 1975), also by Robert N. Desmarais and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TN D-7929 (National Aeronautics and Space Administration ;, 1975), also by Jack D. Leatherwood and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-129 (National Aeronautics and Space Administration ;, 1962), also by G. Louis Smith and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-152 (National Aeronautics and Space Administration ;, 1963), also by Clarence D. Cone and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-153 (National Aeronautics and Space Administration ;, 1963), also by Mitchel H. Bertram, Philip E. Everhart, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-163 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1963), also by Paul W. Huber and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-166 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1963), also by W. Jefferson Stroud and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-167 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1963), also by William L. Grose, Robert L. Trimpi, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-182 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1963), also by Richard D. Wagner, Ralph Watson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-227 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1965), also by David A. Evensen and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-228 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1966), also by Charlie M. Jackson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-247 (National Aeronautics and Space Administration ;, 1966), also by Peter R. Kurzhals, Carolyn Grantham, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-254 (National Aeronautics and Space Administration ;, 1967), also by Richard A. Hord and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-256 (National Aeronautics and Space Administration ;, 1967), also by Herbert J. Cunningham and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-259 (National Aeronautics and Space Administration ;, 1967), also by Paul F. Holloway, E. Brian Pritchard, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-260 (National Aeronautics and Space Administration ;, 1967), also by Paul F. Holloway, E. Brian Pritchard, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-264 (National Aeronautics and Space Administration ;, 1967), also by Wilmer H. Reed and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-266 (National Aeronautics and Space Administration ;, 1967), also by Sherman A. Clevenson, Roy Steiner, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-279 (National Aeronautics and Space Administration ;, 1968), also by Robert G. Thomson and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-282 (National Aeronautics and Space Administration ;, 1968), also by Windsor L. Sherman, Sylvia A. Wallace, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-285 (National Aeronautics and Space Administration ;, 1968), also by Ray H. Wright, Benferd L. Schilling, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-289 (National Aeronautics and Space Administration ;, 1968), also by Frank Hohl and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-295 (National Aeronautics and Space Administration ;, 1968), also by Walter B. Olstad and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-296 (National Aeronautics and Space Administration ;, 1969), also by Harold G. Bush, Marvin B. Dow, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-297 (National Aeronautics and Space Administration ;, 1969), also by John D. Bird and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-298 (National Aeronautics and Space Administration ;, 1969), also by Richard Madden and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-300 (National Aeronautics and Space Administration ;, 1969), also by George W. Jones, Robert W. Walker, Joseph J. Cincotta, George C. Marshall Space Flight Center, Martin Company, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-302 (National Aeronautics and Space Administration ;, 1969), also by Harry H. Heyson and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-311 (National Aeronautics and Space Administration ;, 1969), also by Richard W. Barnwell and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-314 (National Aeronautics and Space Administration ;, 1969), also by John H. Painter, Jon W. Bayless, Someshwar C. Gupta, Southern Methodist University. Institute of Technology, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-317 (National Aeronautics and Space Administration ;, 1969), also by Clarence W. Matthews and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-325 (National Aeronautics and Space Administration ;, 1969), also by Willard E. Meador and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-330 (National Aeronautics and Space Administration ;, 1970), also by R. W. Hess and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-331 (National Aeronautics and Space Administration ;, 1970), also by Constantine A. Balanis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-339 (National Aeronautics and Space Administration ;, 1970), also by Calvin T. Swift and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-344 (National Aeronautics and Space Administration ;, 1970), also by Ray H. Wright, James D. Keller, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-357 (National Aeronautics and Space Administration ;, 1971), also by Perry A. Newman, Robert L. Bowden, Virginia Polytechnic Institute and State University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-363 (National Aeronautics and Space Administration ;, 1971), also by John Q. Howell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-364 (National Aeronautics and Space Administration ;, 1971), also by Harry H. Heyson and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-368 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1971), also by Julius E. Harris and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-374 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1971), also by E. B. Klunker, Ruby M. Davis, Jerry C. South, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-379 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1971), also by James D. Keller, Ray H. Wright, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-57 (National Aeronautics and Space Administration ;, 1960), also by A. I. Neihouse, Stanley H. Scher, Walter J. Klinar, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-58 (National Aeronautics and Space Administration ;, 1960), also by John P. Mugler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-59 (National Aeronautics and Space Administration ;, 1960), also by Elbridge Z. Stowell, George J. Heimerl, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: NASA TR R-62 (National Aeronautics and Space Administration ;, 1960), also by Leonard Roberts and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-63 (National Aeronautics and Space Administration ;, 1960), also by Robert L. Trimpi, Robert A. Jones, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-65 (National Aeronautics and Space Administration ;, 1960), also by Clarence L. Gillis, Charles T. D'Aiutolo, Jesse L. Mitchell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA TR R-71 (National Aeronautics and Space Administration ;, 1960), also by Harry H. Heyson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: NASA-UVa Light Aerospace Alloy and Structures Technology Program supplement : aluminum-based materials for high speed aircraft : semi-annual report July 1, 1992-December 31, 1992 (National Aeronautics and Space Administration, Langley Research Center, 1995), also by E. A. Starke (page images at HathiTrust)
• Langley Research Center: NASA/DOD control/structures interaction technology, 1986 : proceedings of a conference sponsored by NASA Langley Research Center, Hampton, Virginia, and Air Force Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio, and held in Norfolk, Virginia, November 18-21, 1986 (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986), also by Robert L. Wright, Air Force Wright Aeronautical Laboratories, United States Department of Defense, United States National Aeronautics and Space Administration, and Va.) NASA/DOD CSI Technology Conference (1st : 1986 : Norfolk (page images at HathiTrust)
• Langley Research Center: NASA/DOD controls-structures interaction technology, 1989 : proceedings of a conference cosponsored by NASA Langley Research Center, Hampton, Virginia, and Wright Research Development Center, Wright-Patterson Air Force Base, Ohio, and held in San Diego, California, January 29-February 2, 1989 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989), also by Jerry R. Newsom, Wright Research Development Center, and Calif.) NASA/DOD CSI Technical Conference (3rd : 1989 : San Diego (page images at HathiTrust)
• Langley Research Center: NASTRAN user's guide : level 15 (National Aeronautics and Space Administration ;, 1975), also by United States National Aeronautics and Space Administration and Inc Universal Analytics (page images at HathiTrust)
• Langley Research Center: National Aeronautics and Space Administration research on materials applicable to supersonic transports (National Aeronautics and Space Administration ;, 1964), also by Herbert F. Hardrath and George J. Heimerl (page images at HathiTrust)
• Langley Research Center: National Educators' Workshop, update 93 : standard experiments in engineering materials science and technology : proceedings of a workshop sponsored jointly by the National Aeronautics and Space Administration, Washington, D.C.; the Norfolk State University, Norfolk, Virginia; the United States Department of Energy, Oak Ridge, Tennessee; and the National Institute of Standards and Technology, Washington, D.C., and held in Hampton, Virginia, November 3-5, 1993 (National Aeronautics and Space Administration ;, 1994), also by Virg.) National Educators' Workshop: Update '93 (1993 : Hampton, James A. Jacobs, James E. Gardner, Norfolk State University (Va.), National Institute of Standards and Technology (U.S.), United States. Department of Energy, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The natural flow wing-design concept (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Richard M. Wood and Steven X. S. Bauer (page images at HathiTrust)
• Langley Research Center: Natural laminar flow airfoil design considerations for winglets on low-speed airplanes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by C. P. Van Dam and Vigyan Research Associates (page images at HathiTrust)
• Langley Research Center: Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings : a correlation with experiment (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by S. Naomi McMillin, Earll M. Murman, and James L. Thomas (page images at HathiTrust)
• Langley Research Center: A navigation-aids identification decoder and display for general-aviation aircraft (National Aeronautics and Space Administration ;, 1969), also by Charles W. Meissner and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Navigation, guidance, and control for helicopter automatic landings (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by James R. Kelly, Frank R. Niessen, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: The NCOREL computer program for 3D nonlinear supersonic potential flow computations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Michael J. Siclari, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Near-field and far-field noise surveys of solid-fuel rocket engines for a range of nozzle exit pressures (National Aeronautics and Space Administration, 1959), also by William H. Mayes, Harvey H. Hubbard, and Wade E. Lanford (page images at HathiTrust)
• Langley Research Center: Near-field sonic-boom pressure signatures for the space shuttle launch and orbiter vehicles at Mach 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by George C. Ashby and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Near-field testing of the 15-meter hoop-column antenna (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Lyle C. Schroeder (page images at HathiTrust)
• Langley Research Center: Near minimum-time maneuvers of the advanced space structures technology research experiment (ASTREX) test article : theory and experiments (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Srinivas R. Vadali and Michael T. Carter (page images at HathiTrust)
• Langley Research Center: NECAP : NASA's Energy-Cost Analysis Program (National Aeronautics and Space Administration ;, 1975), also by R. H. Henninger and General American Transportation Corporation. Research Division (page images at HathiTrust)
• Langley Research Center: A new approach to aerial combat games (National Aeronautics and Space Administration ;, 1970), also by Sheldon Baron and Beranek Bolt (page images at HathiTrust)
• Langley Research Center: A new approach to the solution of large, full matrix equations : a two-dimensional potential flow feasibility study (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by R. M. James, R. W. Clark, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A new dynamic pressure source for the calibration of pressure transducers (U.S. Dept. of Commerce, National Bureau of Standards, Institute for Applied Technology, 1976), also by Carol F. Vezzetti and Institute for Applied Technology (U.S.). Electronic Technology Division (page images at HathiTrust)
• Langley Research Center: A new field-laboratory methodology for assessing human response to noise (National Aeronautics and Space Administration ;, 1973), also by Paul N. Borsky and Columbia University (page images at HathiTrust)
• Langley Research Center: A new look at numerical analyses of free-edge stresses in composite laminates (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by I. S. Raju, J. G. Goree, J. D. Whitcomb, Joint Institute for Advancement of Flight Sciences, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A new matrix theorem and its application for establishing independent coordinates for complex dynamical systems with constraints (National Aeronautics and Space Administration, 1969), also by William C. Walton and Earl C. Steeves (page images at HathiTrust)
• Langley Research Center: New technique for experimental generation of two-dimensional blade-vortex interaction at low Reynolds numbers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Earl R. Booth and James C. Yu (page images at HathiTrust)
• Langley Research Center: A new theory for rapid calculation of the ground pattern of the incident sound intensity produced by a maneuvering jet airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Raymond L. Barger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: New triangular and quadrilateral plate-bending finite elements (National Aeronautics and Space Administration ;, 1974), also by R. Narayanaswami (page images at HathiTrust)
• Langley Research Center: Noise and wake structure measurements in a subsonic tip speed fan (National Aeronautics and Space Administration ;, 1973), also by B. Magliozzi and United Aircraft Corporation. Hamilton Standard Division (page images at HathiTrust)
• Langley Research Center: Noise characteristics of jet flap type exhaust flows (National Aeronautics and Space Administration ;, 1974), also by G. O. Schrecker, J. R. Maus, and University of Tennessee (System). Space Institute (page images at HathiTrust)
• Langley Research Center: Noise characteristics of upper surface blown configurations : analytical studies (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Narayana N. Reddy, and Lockheed-Georgia Company (page images at HathiTrust)
• Langley Research Center: Noise data for a twin-engine commercial jet aircraft flying conventional, steep, and two-segment approaches (National Aeronautics and Space Administration ;, 1977), also by Earl C. Hastings, J. R. Hamilton, Arnold W. Mueller, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Noise measurements for a three-engine turbofan transport airplane during climbout and landing approach operations (U.S. National Aeronautics and Space Administration ;, 1971), also by W. Latham Copeland, Lorenzo R. Clark, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Noise measurements for a twin-engine commercial jet aircraft during 3 degree approaches and level flyovers (U.S. National Aeronautics and Space Administration ;, 1976), also by Earl C. Hastings, Arnold W. Mueller, Robert E. Shanks, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Noise of a model helicopter rotor due to ingestion of turbulence (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Robert W. Paterson, Roy K. Amiet, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Noise reduction by means of inlet-guide-vane choking in an axial-flow compressor (National Aeronautics and Space Administration, 1968), also by David Chestnutt and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Noise reduction in a Mach 5 wind tunnel with a rectangular rod-wall sound shield (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Theodore R. Creel, Ivan E. Beckwith, J. Wayne Keyes, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Noise suppression characteristics of peripherally segmented duct liners (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Willie R. Watson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Noise suppression with high Mach number inlets (U.S. National Aeronautics and Space Administration ;, 1976), also by Edward Lumsdaine, Jenn G. Cherng, Ismail Tag, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Noise transmission loss of a rectangular plate in an infinite baffle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Louis A. Roussos (page images at HathiTrust)
• Langley Research Center: Noise transmission loss of aircraft panels using acoustic intensity methods (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Michael C. McGary and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Noise transmission through flat rectangular panels into a closed cavity (National Aeronautics and Space Adinistration, Scientific and Technical Information Office ;, 1978), also by C. Kearney Barton, Edward F. Daniels, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: The noisiness of low-frequency one-third octave bands of noise (National Aeronautics and Space Administration ;, 1975), also by Ben William Lawton (page images at HathiTrust)
• Langley Research Center: Non-engine aerodynamic noise investigation of a large aircraft (National Aeronautics and Space Administration ;, 1974), also by J. S. Gibson and Lockheed-Georgia Company (page images at HathiTrust)
• Langley Research Center: Nonaqueous slip casting of YBa2Cu3O7-x superconductive ceramics (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Matthew W. Hooker and Theodore D. Taylor (page images at HathiTrust)
• Langley Research Center: Nondestructive testing of Scout rocket motors (National Aeronautics and Space Administration ;, 1972), also by Arthur E. Oaks and General Electric Company (page images at HathiTrust)
• Langley Research Center: Nonlinear acoustic theory for rigid porous materials (National Aeronautics and Space Administration ;, 1971), also by W. E. Zorumski, Tony L. Parrott, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Nonlinear actuator disk theory and flow field calculations, including nonuniform loading (National Aeronautics and Space Administration ;, 1970), also by Michael D. Greenberg, Stephen R. Powers, and Inc Sage Action (page images at HathiTrust)
• Langley Research Center: Nonlinear modeling of joint dominated structures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by J. C. Chapman and Boeing Aerospace Company. Engineering Technology (page images at HathiTrust)
• Langley Research Center: Nonlinear programming extensions to rational function approximation methods for unsteady aerodynamic forces (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Sherwood H. Tiffany and William M. Adams (page images at HathiTrust)
• Langley Research Center: A nonlinear structural concept for compliant walls (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Edward L. Reiss, Applied Institute of Mathematics, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A nonlinear theory for airfoils with trailing-edge jet flap (National Aeronautics and Space Administration ;, 1976), also by Raymond L. Barger and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A Nonlinear theory for predicting the effects of unsteady laminar, turbulent, or transitional boundary layers on the attenuation of shock waves in a shock tube with experimental comparison (U.S. G.P.O., 1961), also by Robert L. Trimpi, Nathaniel B. Cohen, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Nonmetallic materials handbook (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Stanley E. Podlaseck and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Nonparallel instability of supersonic and hypersonic boundary layers (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Nabil M. El-Hady and Inc Analytical Services & Materials (page images at HathiTrust)
• Langley Research Center: Nonparallel stability of three-dimensional compressible boundary layers (National Aeronautics and Space Administration, Scientifice and Technical Information Office ;, 1980), also by Nabil M. El-Hady and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Nonreactive mixing study of a scramjet swept-strut fuel injector (National Aeronautics and Space Administration ;, 1975), also by Charles R. McClinton (page images at HathiTrust)
• Langley Research Center: A note on the calculation of helicopter performance at high tip-speed ratios (National Aeronautics and Space Administration, 1959), also by Alfred Gessow (page images at HathiTrust)
• Langley Research Center: A note on the determination of the gravitational constant k. (Engineering Experiment Station, Georgia Institute of Technology], 1961), also by Eugene Lemuel Davis and Seminar on Celestial Mechanics (1961) (page images at HathiTrust; US access only)
• Langley Research Center: A note on the mean value of induced velocity for a helicopter rotor (National Aeronautics and Space Administration, 1960), also by Harry H. Heyson (page images at HathiTrust)
• Langley Research Center: Nozzle development and physical site alternation (National Aeronautics and Space Administration ;, 1973), also by G. L. Romine, J. Gliozzi, T. D. Reisert, and Martin Marietta Corporation (page images at HathiTrust)
• Langley Research Center: Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Theodore R. Creel, Fang-Jenq Chen, and Ivan E. Beckwith (page images at HathiTrust)
• Langley Research Center: NR-150B2 adhesive development (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by P. S. Blatz and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Nuclear-fragmentation studies for microelectronic applications (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by M. Ngo Duc (page images at HathiTrust)
• Langley Research Center: Nucleon and heavy-ion total and absorption cross section for selected nuclei (National Aeronautics and Space Administration ;, 1975), also by John W. Wilson and Christopher M. Costner (page images at HathiTrust)
• Langley Research Center: Numerical analysis and parametric studies of the buckling of composite orthotropic compression and shear panels (National Aeronautics and Space Administration ;, 1975), also by Jerrold M. Housner and Manuel Stein (page images at HathiTrust)
• Langley Research Center: Numerical analysis and simulation of an assured crew return vehicle flow field (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by K. James Weilmuenster, Francis A. Greene, and Robert E. Smith (page images at HathiTrust)
• Langley Research Center: Numerical analysis of the scramjet-inlet flow field by using two-dimensional Navier-Stokes equations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Ajay Kumar and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Numerical and experimental studies of the natural convection within a horizontal cylinder (National Aeronautics and Space Administration ;, 1974), also by Roger B. Stewart, Lillian R. Boney, and Alexander P. Sabol (page images at HathiTrust)
• Langley Research Center: Numerical calculations of velocity and pressure distribution around oscillating airfoils (National Aeronautics and Space Administration ;, 1974), also by Theodore Bratanow, Michael Kobiske, Akin Ecer, and University of Wisconsin--Milwaukee (page images at HathiTrust)
• Langley Research Center: Numerical computation of transonic flows by finite-element and finite-diffence methods (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, M. M. Hafez, and inc Flow Research (page images at HathiTrust)
• Langley Research Center: Numerical grid generation techniques : proceedings of a workshop (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Institute for Computer Applications in Science and Engineering, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Numerical grid generation techniques : proceedings of a workshop held at NASA Langley Research Center, Hampton, Virginia, October 6-7, 1980 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Institute for Computer Applications in Science and Engineering and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A numerical method for evaluation and utilization of supersonic nacelle-wing interference (National Aeronautics and Space Administration :, 1969), also by Robert J. Mack and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles : part 2 - applications (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by P. D. Thomas and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles : theory (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by P. D. Thomas and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Numerical methods for the design and analysis of wings at supersonic speeds (National Aeronautics and Space Administration ;, 1974), also by Harry W. Carlson and David S. Miller (page images at HathiTrust)
• Langley Research Center: Numerical modeling tools for chemical vapor deposition (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1992), also by Thomas John Jasinski, Edwards P. Childs, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: Numerical optimization techniques for bound circulation distribution for minimum induces drag of nonplanar wings : basic formulations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by John Kuhlman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Numerical procedure to determine geometric view factors for surfaces occluded by cylinders (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Patricia L. Sawyer and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1989), also by F. F. Badavi (page images at HathiTrust)
• Langley Research Center: Numerical simulation of channel flow transition : resolution requirements and structure of the hairpin vortex (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Steven E. Krist and Thomas A. Zang (page images at HathiTrust)
• Langley Research Center: Numerical simulation of three dimensional .... (National Aeronautics and Space Administration, Langley Research Center ;, 1993), also by John V. Shebalin (page images at HathiTrust)
• Langley Research Center: Numerical solution of supersonic three-dimensional free-mixing flows using the parabolic ellipit Navier-Stokes equations (National Aeronautics and Space Administration ;, 1976), also by Richard Hirsch and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Numerical solution of the hypersonic viscous-shock-layer equations for laminar, transitional, and turbulent flows of a perfect gas over blunt axially symmetric bodies (National Aeronautics and Space Administration ;, 1975), also by E. Clay Anderson and James N. Moss (page images at HathiTrust)
• Langley Research Center: Numerical solutions of the Navier-Stokes equations for the supersonic laminar flow over a two-dimensional compression corner (National Aeronautics and Space Administration ;, 1972), also by James E. Carter (page images at HathiTrust)
• Langley Research Center: Numerical solutions of the Navier-Stokes equations for transonic afterbody flows (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1980), also by R. Charles Swanson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Numerical studies of convective cooling for a locally heated skin (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Stephen J. Scotti (page images at HathiTrust)
• Langley Research Center: Numerical studies of laminar and turbulent drag reduction (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by R. Balasubramanian, Steven A. Orszag, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Numerical studies of laminar and turbulent drag reduction : part II (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by R. Balasubramanian, Steven A. Orszag, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Numerical studies of the deposition of material released from fixed and rotary wing aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), also by Alan J. Bilanin, Milton E. Teske, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A numerical study of electromagnetic scattering from ocean-like surfaces (National Aeronautics and Space Administration ;, 1972), also by R. R. Lentz and Ohio State University (page images at HathiTrust)
• Langley Research Center: Numerical study of sound propagation in a jet flow (National Aeronautics and Space Administration ;, 1975), also by Sharon L. Padula and Chen-Huei Liu (page images at HathiTrust)
• Langley Research Center: Numerical study of the aerodynamic effects of using sulfur hexafluoride as a test gas in wind tunnels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by W. Kyle Anderson (page images at HathiTrust)
• Langley Research Center: A numerical study of transition control by periodic suction-blowing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Sedat Biringen (page images at HathiTrust)
• Langley Research Center: A numerical technique for calculation of the noise of high-speed propellers with advanced blade geometry (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Paul A. Nystrom, F. Farassat, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Oculometric indices of simulator and aircraft motion (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by James R. Comstock, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Old Dominion University (page images at HathiTrust)
• Langley Research Center: ODIN : Optimal Design Integration System (National Aeronautics and Space Administration ;, 1975), also by C. R. Glatt, D. S. Hague, and Aerophysics Research Corporation (page images at HathiTrust)
• Langley Research Center: Oil-flow study of a space shuttle orbiter tip-fin controller (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by V. T. Helms (page images at HathiTrust)
• Langley Research Center: On-board multispectral classification study (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by D. Ewalt and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: On chemical reactions in the char zone during ablation (National Aeronautics and Space Administration ;, 1971), also by Gary C. April, Eduardo Gonzalez Del Valle, Ralph W. Pike, and La.) Louisiana State University (Baton Rouge (page images at HathiTrust)
• Langley Research Center: On lateral cable oscillations of cable-connected space stations (National Aeronautics and Space Administration ;, 1969), also by Willard W. Anderson (page images at HathiTrust)
• Langley Research Center: On-line mass spectrometric monitoring of the polymerization of a phenolic-resin-based material (National Aeronautics and Space Administration ;, 1975), also by David A. Aikens, Billy T. Upchurch, and George M. Wood (page images at HathiTrust)
• Langley Research Center: On minimizing the number of calculations in design-by-analysis codes (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Raymond L. Barger and Anutosh Moitra (page images at HathiTrust)
• Langley Research Center: On-orbit structural dynamic performance of a 15-meter microwave radiometer antenna (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Deborah M. Wahls, David W. Sleight, and Jeffery T. Farmer (page images at HathiTrust)
• Langley Research Center: On the effect of boundary layer growth on the stability of compressible flows (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Nabil M. El-Hady and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: On the formulation of a minimal uncertainty model for robust control with structured uncertainty (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Christine M. Belcastro, Robert Fischl, and B. -C. Chang (page images at HathiTrust)
• Langley Research Center: On the generation of side-edge flap noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by M. S. Howe and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: On the logarithmic-singularity correction in the kernel function method of subsonic lifting-surface theory (National Aeronautics and Space Administration ;, 1977), also by C. Edward Lan, John E. Lamar, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: On the question of instabilities upstream of cylindrical bodies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Mark V. Morkovin and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: On the radiation of a magnetic line source excited cylinder through an axially slotted plasma sheath (National Aeronautics and Space Administration ;, 1967), also by Andrejs Olte, University of Michigan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: On the stability and pointing of an attached double-gimbal experiment package (National Aeronautics and Space Administration, 1972), also by Nelson J. Groom, John D. Shaughnessy, Vilas D. Nene, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: On the theory of compliant wall drag reduction in turbulent boundary layers (National Aeronautics and Space Administration, 1974), also by Robert L. Ash and Old Dominion University (page images at HathiTrust)
• Langley Research Center: On the use of a magnetometer to determine the angular motion of a spinning body in regular precession (National Aeronautics and Space Administration :, 1964), also by George R. Young and Jesse D. Timmons (page images at HathiTrust)
• Langley Research Center: On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently (National Aeronautics and Space Administration ;, 1974), also by Raymond L. Barger (page images at HathiTrust)
• Langley Research Center: On the various forms of the energy equation for a dilute, monatomic mixture of nonreacting gases (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Christopher A. Kennedy (page images at HathiTrust)
• Langley Research Center: On the wall-normal velocity of the compressible boundary-layer equations (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by C. David Pruett and Inc Analytical Services and Materials (page images at HathiTrust)
• Langley Research Center: One-dimensional numerical analysis of the transient thermal response of multilayer insulative systems (U.S. National Aeronautics and Space Administration ;, 1976), also by C. M. Pittman, Kay L. Brinkley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Robert M. Hall and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Operating characteristics of the Langley Mach 10 high Reynolds number helium tunnel (National Aeronautics and Space Administration ;, 1974), also by Ralph D. Watson, Michael C. Fischer, and Dana J. Morris (page images at HathiTrust)
• Langley Research Center: Operating characteristics of the Langley Mach 7 Scramjet Test Facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Robert W. Guy and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Bobby L. Berrier, Linda S. Bangert, and Laurence D. Leavitt (page images at HathiTrust)
• Langley Research Center: Operational considerations in utilization of microwave landing system approach and landing guidance (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by William F. White, Leonard V. Clark, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Operational evaluation of a propeller test stand in the quiet flow facility at Langley Research Center (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by P. J. W. Block and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Operational experiences of a commercial helicopter flown in a large metropolitan area (National Aeronautics and Space Administration ;, 1975), also by Daniel J. DiCarlo (page images at HathiTrust)
• Langley Research Center: Operator strategies under varying conditions of workload (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Ruth J. Arnegard and Old Dominion University. Dept. of Psychology (page images at HathiTrust)
• Langley Research Center: Optical analysis of a compound quasi-microscope for planetary landers (National Aeronautics and Space Administration ;, 1974), also by Stephen D. Wall, Friedrich O. Huck, and Ernest E. Burcher (page images at HathiTrust)
• Langley Research Center: Optical-model abrasion cross sections for high-energy heavy ions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Lawrence W. Townsend and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Optical propagation measurements at Emerson Lake - 1968 (National Aeronautics and Space Administration, 1971), also by Gus E. Mevers, David L. Fried, Melvin P. Keister, United States National Aeronautics and Space Administration, and North American Rockwell Corp (page images at HathiTrust)
• Langley Research Center: Optical radar measurements of the atmosphere (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1967), also by James D. Lawrence, Michael P. McCormick, Frederic Rudolph Crownfield, and College of William and Mary (page images at HathiTrust)
• Langley Research Center: Optically coupled digital altitude encoder for general aviation altimeters (National Aeronautics and Space Administration ;, 1975), also by Floyd R. Bryant (page images at HathiTrust)
• Langley Research Center: Optimal and suboptimal control technique for aircraft spin recovery (National Aeronautics and Space Administration ;, 1974), also by John W. Young (page images at HathiTrust)
• Langley Research Center: Optimal control problems as equivalent Lagrange problems (National Aeronautics and Space Administration ;, 1970), also by Stephen Keith Park and North Carolina State University (page images at HathiTrust)
• Langley Research Center: Optimal control problems with switching points (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Hans Seywald and Virginia Polytechnic Institute and State University. Interdisciplinary Center for Applied Mathematics (page images at HathiTrust)
• Langley Research Center: Optimal guidance law development for an advanced launch system (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by Anthony J. Calise and Martin S. K. Leung (page images at HathiTrust)
• Langley Research Center: Optimal regulation in systems with stochastic time sampling (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Raymond C. Montgomery, Peter S. Lee, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Optimal singular control with applications to trajectory optimization (National Aeronautics and Space Administration, Scientific and Technical Office ;, 1979), also by Nguyen X. Vinh, University of Michigan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: An optimality criterion for sizing members of heated structures with temperature constraints (National Aeronautics and Space Administration ;, 1977), also by G. Venkateswara Rao, R. Narayanaswami, Charles P. Shore, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Optimization of composite sandwich cover panels subjected to compressive loadings (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Juan R. Cruz (page images at HathiTrust)
• Langley Research Center: Optimized resolved rate control of seven-degree-of-freedom Laboratory Telerobotic Manipulator (LTM) with application to three-dimensional graphics simulation (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by L. Keith Barker and William S. McKinney (page images at HathiTrust)
• Langley Research Center: Optimizing interplanetary trajectories with deep space maneuvers (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), also by John Navagh and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: Optimum design of insulated tension members subjected to aerodynamic heating (National Aeronautics and Space Administration, 1959), also by John R. Davidson (page images at HathiTrust)
• Langley Research Center: Optimum proportions of truss-core and web-core sandwich plates loaded in compression (National Aeronautics and Space Administration, 1959), also by Melvin S. Anderson (page images at HathiTrust)
• Langley Research Center: Optimum reentry trajectories of a lifting vehicle (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Jeng-Shing Chern, Nguyen X. Vinh, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: ORACLS - a system for linear-quadratic-gaussian control law design (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Ernest S. Armstrong and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Orbit dynamics and geographical coverage capabilities of satellite-based solar occultation experiments for global monitoring of stratospheric constituents (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by David R. Brooks and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: The orbital mechanics of flight mechanics. (Scientific and Technical Information Office, National Aeronautics and Space Administration; [for sale by the National Technical Information Service, Springfield, Va.], 1973), also by Robert Scott Dunning (page images at HathiTrust)
• Langley Research Center: Ordinates and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively (U.S. G.P.O., 1961), also by Elizabeth W. Patterson, Albert L. Braslow, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Elizabeth B. Plentovich and Blair B. Gloss (page images at HathiTrust)
• Langley Research Center: Osmotically induced coalescence of sarcoma cells through intercellular bridges in vitro (National Aeronautics and Space Administration ;, 1969), also by Clarence D. Cone and Max Tongier (page images at HathiTrust)
• Langley Research Center: Oxidation and emittance of superalloys in heat shield applications (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Karl E. Wiedemann, Jalaiah Unnam, and Ronald K. Clark (page images at HathiTrust)
• Langley Research Center: Oxidation characteristics of Ti-14Al-21Nb alloy (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Sankara Narayan Sankaran (page images at HathiTrust)
• Langley Research Center: Oxidation characteristics of Ti-25Al-10Nb-3V-1Mo intermetallic alloy (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Terryl A. Wallace (page images at HathiTrust)
• Langley Research Center: Ozone trend detectability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Janet W. Campbell, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Colo.) Symposium on Ozone Trend Detectability (1977 : Boulder (page images at HathiTrust)
• Langley Research Center: Packaging, delpoyment, and on-orbit assembly options for large geostationary spacecraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by William T. Davis and Charles B. King (page images at HathiTrust)
• Langley Research Center: PAGEOS Project compilation of information for use of experimenter (National Aeronautics and Space Administration ;, 1967), also by David E. Bowker (page images at HathiTrust)
• Langley Research Center: Panel flutter tests on full-scale X-15 lower vertical stabilizer at Mach number of 3.0 (National Aeronautics and Space Administration, 1962), also by Herman L. Bohon and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Parachute-deployment-parameter identification based on an analytical simulation of Viking BLDT AV-4 (National Aeronautics and Space Administration ;, 1974), also by Theodore A. Talay (page images at HathiTrust)
• Langley Research Center: A parallel variable metric optimization algorithm (National Aeronautics and Space Administration ;, 1973), also by Terry A. Straeter and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Parameters affecting firing time of simultaneously triggered trigatron spark gap switches (National Aeronautics and Space Administration ;, 1969), also by M. D. Williams (page images at HathiTrust)
• Langley Research Center: Parametric analysis of an imaging radar for use as an independent landing monitor (National Aeronautics and Space Administration ;, 1974), also by W. Thomas Bundick (page images at HathiTrust)
• Langley Research Center: A parametric analysis of surface temperatures of paraboloidal solar concentrators in space (National Aeronautics and Space Administration ;, 1969), also by Robert J. Platt (page images at HathiTrust)
• Langley Research Center: Parametric experimental investigation of a scramjet nozzle at Mach 6 with freon and argon or air used for exhaust simulation (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by James M. Cubbage and William J. Monta (page images at HathiTrust)
• Langley Research Center: A parametric study of aliasing error for a narrow field of view scanning radiometer (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Nesim Halyo, Steven T. Stallman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Parametric study of ascent performance of a vertically launched hydrogen-fueled single-stage reusable transport (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by John J. Rehder and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A parametric study of cut-off corrugated surface properties (National Aeronautics and Space Administration ;, 1973), also by C. A. Mentzer, L. Peters, and Ohio State University (page images at HathiTrust)
• Langley Research Center: A parametric study of effect of forebody shape on flow angularity at Mach 8 (National Aeronautics and Space Administration ;, 1974), also by Charles B. Johnson and Don C. Marcum (page images at HathiTrust)
• Langley Research Center: Parametric study of microwave-powered high-altitude airplane platforms designed for linear flight (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Charles E. K. Morris and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A parametric study of planform and aeroelastic effects on aerodynamic center, [alpha]- and q-stability derivatives : summary report (National Aeronautics and Space Administration ;, 1973), also by Jan Roskam, C. Edward Lan, and University of Kansas (page images at HathiTrust)
• Langley Research Center: Parametric study of relaminarization of turbulent boundary layers on nozzle walls (National Aeronautics and Space Administration ;, 1974), also by J. P. Kreskovsky, H. McDonald, S. J. Shamroth, and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
• Langley Research Center: A parametric study of the aerodynamic characteristics of nose-cylinder-flare bodies at a Mach number of 6.0 (National Aeronautics and Space Administration ;, 1965), also by George C. Ashby and Aubrey M. Cary (page images at HathiTrust)
• Langley Research Center: Parametric study of variation in cargo-airplane performance related to progression from current to spanloader designs (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Thomas A. Toll and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Parametric trade studies on a Shuttle II launch system architecture (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Douglas O. Stanley (page images at HathiTrust)
• Langley Research Center: The passage of an infinite swept airfoil through an oblique gust (National Aeronautics and Space Administration ;, 1974), also by John J. Adamczyk and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
• Langley Research Center: Passive control of wing/store flutter (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Wilmer H. Reed, Jerome T. Foughner, F. W. Cazier, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Pavement grooving and traction studies; [papers]. (Technology Utilization Division, National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1969), also by Conference on Pavement Grooving and Traction Studies (1968 : Langley Research Center) and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: Payload vibration data measured during five flights of a two-stage solid-propellant launch vehicle (National Aeronautics and Space Administration, 1962), also by Sherman A. Clevenson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: PCSYS, the optimal design integation system picture drawing system with hidden line algorithm capability for aerospace vehicle configurations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by D. S. Hague, J. D. Vanderburg, Aerophysics Research Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Peer review of a formal verification/design proof methodology : summary of a sub-working-group meeting (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985) (page images at HathiTrust)
• Langley Research Center: Perceived noisiness under anechoic, semi-reverberant and earphone listening conditions (National Aeronautics and Space Administration ;, 1972), also by Frank R. Clarke, Karl D. Kryter, and Stanford Research Institute (page images at HathiTrust)
• Langley Research Center: A performance analysis of the optical-mechanical scanner as an imaging system for planetary landers (National Aeronautics and Space Administration ;, 1969), also by Friedrich O. Huck, Jules J. Lambiotte, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Performance and noise generation studies of supersonic air ejectors (National Aeronautics and Space Administration ;, 1972), also by P. S. Barna and Old Dominion University (page images at HathiTrust)
• Langley Research Center: Performance characteristics of a preformed elliptical parachute at altitudes between 200,000 and 100,000 feet obtained by in-flight photography (National Aeronautics and Space Administration :, 1964), also by Charles H. Whitlock and Harold N. Murrow (page images at HathiTrust)
• Langley Research Center: Performance characteristics of a single-engine fighter model fitted with an in-flight thrust reverser (National Aeronautics and Space Administration, 1971), also by Donald L. Maiden, Charles E. Mercer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Performance characteristics of an isolated coannular plug nozzle at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Charles E. Mercer and James R. Burley (page images at HathiTrust)
• Langley Research Center: Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps (National Aeronautics and Space Administration,Scientific and Technical Information Branch ;, 1982), also by Lawrence D. Leavitt, Linda S. Bangert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Performance evaluation of a quasi-microscope for planetary landers (National Aeronautics and Space Administration ;, 1977), also by Ernest E. Burcher and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Performance Evaluation of the Solar Building Test Facility (National Aeronautical and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Ronald N. Jensen and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A performance index approach to aerodynamic design with the use of analysis codes only (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Raymond L. Barger and Anutosh Moitra (page images at HathiTrust)
• Langley Research Center: Performance of 10-kilowatt carbon arc solar radiation simulator (National Aeronautics and Space Administration, 1967), also by Gary C. Goldman and Kenneth Yass (page images at HathiTrust)
• Langley Research Center: Performance of a 26-meter-diameter ringsail parachute in a simulated Martian environment (National Aeronautics and Space Administration ;, 1967), also by Charles H. Whitlock, Lucille C. Coltrane, and Richard J. Bendura (page images at HathiTrust)
• Langley Research Center: Performance of a composite solid propellant at simulated high altitudes (National Aeronautics and Space Administration, 1959), also by Carl C. Ciepluch (page images at HathiTrust)
• Langley Research Center: Performance of a Haynes 188 metallic standoff thermal protection system at Mach 7 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Don E. Avery and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Performance of a hydrogen burner to simulate air entering scramjet combustors (National Aeronautics and Space Administration ;, 1974), also by William Roger Russin (page images at HathiTrust)
• Langley Research Center: Performance of a hypersonic hot fuselage structure with a carbon dioxide frost protected, nonintegral cryogenic tank (National Aeronautics and Space Administration ;, 1975), also by Ellsworth L. Sharpe and L. Robert Jackson (page images at HathiTrust)
• Langley Research Center: Performance of an aircraft tire under cyclic braking and of a currently operational antiskid braking system (National Aeronautics and Space Administration ;, 1972), also by John A. Tanner and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Performance of an isolated two-dimensional variable-geometry wedge nozzle with translating shroud and collapsing wedge at speeds up to Mach 2.01 (National Aeronautics and Space Administration ;, 1975), also by Donald L. Maiden (page images at HathiTrust)
• Langley Research Center: Performance of an isolated two-dimensional wedge nozzle with fixed cowl and variable wedge centerbody at mach numbers up to 2.01 (National Aeronautics and Space Administration ;, 1976), also by Donald L. Maiden and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Performance of an optimized rotor blade at off-design flight conditions (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Aditi Chattopadhyay and Inc Analytical Services & Materials (page images at HathiTrust)
• Langley Research Center: Performance of computer-designed small-size multistage depressed collectors for a high-perveance traveling wave tube (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Peter Ramins and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Performance of LI-1542 reusable surface insulation system in a hypersonic stream (U.S. National Aeronautics and Space Administration ;, 1976), also by L. Roane Hunt, Irving Weinstein, and John L. Shideler (page images at HathiTrust)
• Langley Research Center: Performance of three ablation materials during simulation of long-duration afterbody heating (National Aeronautics and Space Administration ;, 1967), also by Marvin B. Dow and Stephen S. Tompkins (page images at HathiTrust)
• Langley Research Center: Performance of twin two-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20 (National Aeronautics and Space Administration ;, 1977), also by Francis J. Capone, Donald L. Maiden, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Performance, physiological, and oculometer evaluation of VTOL landing displays (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by R. A. North, S. P. Stackhouse, K. Graffunder, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Performance potential of an advanced technology Mach 3 turbojet engine installed on a conceptual high-speed civil transport (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Shelby J. Morris, Peter G. Coen, and Karl A. Geiselhart (page images at HathiTrust)
• Langley Research Center: Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep (National Aeronautics and Space Administration, 1960), also by Arvo A. Luoma, William J. Alford, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Performance test of laser velocimeter system for the Langley 16-Foot Transonic Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by James F. Meyers and United States. Army Aviation Systems Command. Aerostructures Directorate (page images at HathiTrust)
• Langley Research Center: Permeation of oxygen through high purity, large grain silver (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by R. A. Outlaw, Gar B. Hoflund, and W. K. Peregoy (page images at HathiTrust)
• Langley Research Center: Perspective on the span-distributed-load concept for application to large cargo aircraft design (National Aeronautics and Space Administration ;, 1975), also by Allen H. Whitehead (page images at HathiTrust)
• Langley Research Center: Phase change indicators for subambient temperatures (National Aeronautics and Space Administration ;, 1970), also by D. R. Kasanof, E. Kimmel, and Tempil Corporation (page images at HathiTrust)
• Langley Research Center: Phase control during reconstruction of holographically recorded flow fields using real-time holographic interferometry (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Alpheus W. Burner, William K. Goad, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Photoexcitation of lasers and chemical reactions for NASA missions : a theoretical study (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Ali Javan, Michael Guerra, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Laser Development Corporation (page images at HathiTrust)
• Langley Research Center: Photogrammetric technique using entrained balloons for in-flight ranging of trailing vortices (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by W. L. Snow, William K. Goad, and Alpheus W. Burner (page images at HathiTrust)
• Langley Research Center: Photographic atlas of the Moon (Scientific and Technical Information Office, National Aeronautics and Space Administration ;, 1971), also by David E. Bowker, J. Kenrick Hughes, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust; US access only)
• Langley Research Center: Photographic survey of the LDEF mission (National Aeronautics and Space Administration, Langley Research Center, 1996), also by Robert L. O'Neal, Carol C. Kiser, and Arlene S. Levine (page images at HathiTrust)
• Langley Research Center: A photometric function for diffuse reflection by particulate materials (National Aeronautics and Space Administration ;, 1975), also by Willard E. Meador (page images at HathiTrust)
• Langley Research Center: Photometry of an iron artificial meteor reentering at 11 kilometers per second (National Aeronautics and Space Administration ;, 1968), also by James B. Robertson and Wendell G. Ayers (page images at HathiTrust)
• Langley Research Center: Photometry of spectrograms of three artificial meteors (National Aeronautics and Space Administration ;, 1967), also by Gale A. Harvey and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A photovoltaic solar sensor for use in spacecraft orientation control systems (National Aeronautics and Space Administration ;, 1966), also by Anthony Fontana (page images at HathiTrust)
• Langley Research Center: Physically weighted approximations of unsteady aerodynamic forces using the minimum-state method (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Mordechay Karpel and Sherwood T. Hoadley (page images at HathiTrust)
• Langley Research Center: Pilot assessment of two computer generated display formats for helicopter instrument approach (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Frank R. Niessen, James M. Patton, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Pilot evaluation of sailplane handling qualities (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by A. G. Bennett and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Pilot model expansion tunnel test flow properties obtained from velocity, pressure, and probe measurements (National Aeronautics and Space Administration ;, 1973), also by Wilfred J. Friesen, John A. Moore, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Pilot opinions on high level flight deck automation issues : toward the development of a design philosophy (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by Yvette J. Tenney, Richard W. Pew, William H. Rogers, and BBN Systems and Technologies Corporation (page images at HathiTrust)
• Langley Research Center: A piloted fixed-base simulator study of low-speed flight characteristics of an arrow-wing supersonic transport design (National Aeronautics and Space Administration ;, 1968), also by William D. Grantham and Perry L. Deal (page images at HathiTrust)
• Langley Research Center: Piloted simulation of an algorithm for onboard control of time-optimal intercept (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Douglas B. Price, Daniel D. Moerder, and Anthony J. Calise (page images at HathiTrust)
• Langley Research Center: Piloted simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Jay M. Brandon, Alfred J. Wunschel, and Philip W. Brown (page images at HathiTrust)
• Langley Research Center: Piloted simulation study of the effects of an automatic trim system on flight characteristics of a light twin-engine airplane with one engine inoperative (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Eric C. Stewart, Kenneth R. Yenni, and Philip W. Brown (page images at HathiTrust)
• Langley Research Center: Piloted simulator study of allowable time delay in pitch flight control system of a transport airplane with negative static stability (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by William D. Grantham (page images at HathiTrust)
• Langley Research Center: Piloted simulator study of allowable time delays in large-airplane response (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by William D. Grantham (page images at HathiTrust)
• Langley Research Center: Pitot pressure measurements in flow fields behind circular-arc nozzles with exhaust jets at subsonic free-stream mach numbers (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Mary L. Mason, Lawrence E. Putnam, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Planar equations of rollout motion for an aircraft with free or steerable landing gears (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Robert K. Sleeper and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Planform curvature effects on flutter characteristics of a wing with 56 ̊leading-edge sweep and panel aspect ratio of 1.14 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Donald F. Keller, Theresa L. Pinkerton, and M. C. Sandford (page images at HathiTrust)
• Langley Research Center: Planform effects on the supersonic aerodynamics of multibody configurations (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by S. Naomi McMillin and Richard M. Wood (page images at HathiTrust)
• Langley Research Center: Planning fuel-conservative descents in an airline environment using a small programmable calculator : algorithm development and flight test results (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Charles E. Knox, David A. Simmon, and Dan D. Vicroy (page images at HathiTrust)
• Langley Research Center: PLANS : a finite element program for nonlinear analysis of structures. Volume I, Theoretical manual (National Aeronautics and Space Administration, 1975), also by A. Pifko, Harry Armen, H. S. Levine, and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Plasma acceleration by use of guided microwaves (National Aeronautics and Space Administration, 1959), also by Robert V. Hess and Karlheinz Thom (page images at HathiTrust)
• Langley Research Center: Plasma core reactor simulations using RF uranium seeded argon discharges (U.S. National Aeronautics and Space Administration ;, 1976), also by W. C. Roman, United States National Aeronautics and Space Administration, and United Technologies Research Center (page images at HathiTrust)
• Langley Research Center: Plenum response to simulated disturbances of the model and fan inlet guide vanes in a transonic tunne (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Blair B. Gloss (page images at HathiTrust)
• Langley Research Center: Pogo suppression on space shuttle : early studies (National Aeronautics and Space Administration ;, 1973), also by Stanley G. Rubin, J. G. Payne, W. G. Wagner, and Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Point and path performance of light aircraft : a review and analysis (National Aeronautics and Space Administration ;, 1973), also by Frederick O. Smetana, W. Donald Johnson, Delbert C. Summey, and North Carolina State University (page images at HathiTrust)
• Langley Research Center: Pollutant emissions from flat-flame burners at high pressures (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Howard G. Maahs, Irvin M. Miller, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Polynomial approximations of thermodynamic properties of arbitrary gas mixtures over wide pressure and density ranges (National Aeronautics and Space Administration ;, 1972), also by Dennis O. Allison (page images at HathiTrust)
• Langley Research Center: Position paper on the potential of inadvertent weather modification of the Florida peninsula resulting from neutralization of space shuttle solid rocket booster exhaust clouds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Eugene Bollay (page images at HathiTrust)
• Langley Research Center: Positron lifetime measurements in chiral nematic liquid crystals (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Jag J. Singh, Devendra S. Parmar, and Abe Eftekhari (page images at HathiTrust)
• Langley Research Center: Possible modifications to the calculation of perceived noisiness (National Aeronautics and Space Administration, 1970), also by Karl D. Kryter, Stanford Research Institute, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Postbuckling response of long thick isotropic plates loaded in compression including higher order transverse shearing effects (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Manuel Stein, P. Daniel Sydow, and Liviu Librescu (page images at HathiTrust)
• Langley Research Center: Postflight simulation of parachute deployment dynamics of Viking qualification flight tests (National Aeronautics and Space Administration ;, 1973), also by Charles H. Whitlock, Theodore A. Talay, and Lamont R. Poole (page images at HathiTrust)
• Langley Research Center: A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Richard W. Barnwell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Potential problems related to weightlessness and artificial gravity (National Aeronautics and Space Administration ;, 1969), also by Ralph W. Stone, William M. Piland, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Power cepstrum technique with application to model helicopter acoustic data (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by R. M. Martin and C. L. Burley (page images at HathiTrust)
• Langley Research Center: Power-spectral-density relationship for retarded differential equations (National Aeronautics and Space Administration ;, 1974), also by L. Keith Barker (page images at HathiTrust)
• Langley Research Center: Power spectral measurements of clear-air turbulence to long wavelengths for altitudes up to 14 000 meters (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Harold N. Murrow, Richard H. Rhyne, William E. McCain, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: The practical application of a finite difference method for analyzing transonic flow over oscillating airfoils and wings (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by F. Edward Ehlers, James D. Sebastian, Boeing Commercial Airplane Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Practical small-scale explosive seam welding (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Laurence J. Bement and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Predeployment validation of fault-tolerant systems through software-implemented fault insertion (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Edward W. Czeck, Zary Z. Segall, Daniel P. Siewiorek, and Carnegie-Mellon University. Dept. of Electrical and Computer Engineering (page images at HathiTrust)
• Langley Research Center: Predicted characteristics of an inflatable aluminized-plastic spherical earth satellite with regard to temperature, visibility, reflection of radar waves, and protection from ultraviolet radiation (National Aeronautics and Space Administration, 1959), also by George P. Wood and Arlen F. Carter (page images at HathiTrust)
• Langley Research Center: Predicted effect of dynamic load on pitting fatigue life for low-contact-ratio spur gears (National Aeronautics and Space Administration, 1986), also by David G. Lewicki, United States. Army Aviation Systems Command, United States. Army Aviation Research and Technology Activity. Propulsion Directorate, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Predicting failure of specimens with either surface cracks or corner cracks at holes (National Aeronautics and Space Administration ;, 1976), also by J. C. Newman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Prediction and verification of creep behavior in metallic materials and components for the space shuttle thermal protection system : summary report (U.S. National Aeronautics and Space Administration ;, 1976), also by John W. Davis, Bruce A. Cramer, United States National Aeronautics and Space Administration, and McDonnell Douglas Astronautics Company-East (page images at HathiTrust)
• Langley Research Center: Prediction of airframe noise (National Aeronautics and Space Administration ;, 1975), also by Jay C. Hardin (page images at HathiTrust)
• Langley Research Center: Prediction of compliant wall drag reduction, part I (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Steven A. Orszag, inc Cambridge Hydrodynamics, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Prediction of compliant wall drag reduction, part II (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Steven A. Orszag, inc Cambridge Hydrodynamics, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Prediction of effects of wing contour modifications on low-speed maximum lift and transonic performance for the EA-6B aircraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Dennis O. Allison and E. G. Waggoner (page images at HathiTrust)
• Langley Research Center: Prediction of flyover jet noise spectra from static tests (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Ulf Michel, Alfons Michalke, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Prediction of payload vibration environments by mechanical admittance test techniques (National Aeronautics and Space Administration ;, 1975), also by Daniel D. Kana, Luis M. Vargas, and Southwest Research Institute (page images at HathiTrust)
• Langley Research Center: Prediction of rotating-blade vortex noise from noise of nonrotating blades (United States National Aeronautics and Space Administration ;, 1976), also by Martin R. Fink, Roy K. Amiet, Robert H. Schlinker, United States National Aeronautics and Space Administration, and United Technologies Research Center (page images at HathiTrust)
• Langley Research Center: Prediction of subsonic vortex shedding from forebodies with chines (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by M. R. Mendenhall, Daniel J. Lesieutre, and Nielsen Engineering & Research (page images at HathiTrust)
• Langley Research Center: Prediction of the pattern performance for the Aeroassist Flight Experiment (AFE) spacecraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by C. Yang, R. Torres, R. C. Rudduck, and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: Prediction of unsteady aerodynamic loadings caused by leading edge and trailing edge control surface motions in subsonic compressible flow : analysis and results (National Aeronautics and Space Administration ;, 1975), also by W. S. Rowe and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Prediction of unsteady aerodynamic loadings caused by trailing edge control surface motions in subsonic compressible flow : analysis and results (National Aeronautics and Space Administration ;, 1972), also by W. S. Rowe, M. C. Redman, B. A. Winther, and Boeing Company (page images at HathiTrust)
• Langley Research Center: Prediction of Viking lander camera image quality (National Aeronautics and Space Administration ;, 1976), also by Friedrich O. Huck and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Preliminary analysis of a radiobiological experiment for LifeSat (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by John W. Wilson (page images at HathiTrust)
• Langley Research Center: Preliminary analysis of a simulated meteor reentry at 9.8 kilometers per second (National Aeronautics and Space Administration :, 1964), also by W. O. Jewell and Andrew Rugh Wineman (page images at HathiTrust)
• Langley Research Center: Preliminary analysis of the implications of natural radiations on geostationary operations (National Aeronautics and Space Administration ;, 1976), also by John W. Wilson, Fred M. Denn, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Preliminary analysis of the span-distributed-load concept for cargo aircraft design (National Aeronautics and Space Administration ;, 1975), also by Allen H. Whitehead (page images at HathiTrust)
• Langley Research Center: A preliminary assessment of the impact of 2-D exhaust-nozzle geometry on the cruise range of a hypersonic aircraft with top-mounted ramjet propulsion (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Walter A. Vahl, John P. Weidner, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Preliminary calculation of solar cosmic ray dose to the female breast in space missions (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Mark R. Shavers (page images at HathiTrust)
• Langley Research Center: Preliminary design procedure for insulated structures subjected to transient heating (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Howard M. Adelman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Preliminary design study of a lateral-directional control system using thrust vectoring (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Frederick J. Lallman (page images at HathiTrust)
• Langley Research Center: Preliminary development of digital signal processing in microwave radiometers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by William D. Stanley and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Preliminary feasibility analysis of a pressure modulator radiometer for remote sensing of tropospheric constituents (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Harry D. Orr, Pamela L. Rarig, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Preliminary investigation of effect of environmental factors on salt stress corrosion cracking of Ti-8Al-lMO-lV at elevated temperatures (National Aeronautics and Space Administration ;, 1964), also by D. N. Braski (page images at HathiTrust)
• Langley Research Center: A preliminary investigation of the destruction of solid-propellant rocket motors by impact from small particles (National Aeronautics and Space Administration, 1960), also by David J. Carter (page images at HathiTrust)
• Langley Research Center: Preliminary investigation of the handling qualities of a vehicle in a simulated lunar gravitational field (National Aeronautics and Space Administration :, 1965), also by Peter C. Boisseau (page images at HathiTrust)
• Langley Research Center: Preliminary results of compression tests on cylinders with eccentric longitudinal stiffeners (National Aeronautics and Space Administration ;, 1964), also by Michael F. Card (page images at HathiTrust)
• Langley Research Center: Preliminary rotor wake measurements with a laser velocimeter (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Danny R. Hoad, David B. Rhodes, James F. Meyers, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Preliminary study of a large span-distributed-load flying-wing cargo airplane concept (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Lloyd S. Jernell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Preliminary study of a possible automatic landing system (National Aeronautics and Space Administration ;, 1974), also by Windsor L. Sherman and Sylvia W. Winfrey (page images at HathiTrust)
• Langley Research Center: A preliminary study of relaxation methods for the inviscid conservative gasdynamics equations using flux splitting (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Joseph L. Steger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Preliminary surveys of the wall boundary layer in a Mach 6 axisymmetric tunnel (National Aeronautics and Space Administration ;, 1970), also by Robert A. Jones and William V. Feller (page images at HathiTrust)
• Langley Research Center: Preliminary system design study for a digital fly-by-wire flight control system for an F-8C aircraft (National Aeronautics and Space Administration ;, 1976), also by C. L. Seacord, Darrel Vaughn, and Honeywell Inc (page images at HathiTrust)
• Langley Research Center: Premission and postmission simulation studies of the foot-controlled maneuvering unit for Skylab experiment T-020 (National Aeronautics and Space Administration ;, 1975), also by Donald E. Hewes and Kenneth E. Glover (page images at HathiTrust)
• Langley Research Center: Preparation and characterization of low DP end-capped Pyrrone moldings (National Aeronautics and Space Administration ;, 1970), also by Charles T. Hughes and Avco Corporation. Systems Division (page images at HathiTrust)
• Langley Research Center: Preparation and properties of imide/pyrrone copolymers (National Aeronautics and Space Administration ;, 1969), also by Vernon Lee Bell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by David S. Miller and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Pressure and heat-transfer distributions in a simulated wing-elevon cove with variable leakage at a free-stream Mach number of 6.9 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by William D. Deveikis, Whitney Bartlett, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Pressure data for four analytically defined arrow wings in supersonic flow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by James C. Townsend and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range (National Aeronautics and Space Administration ;, 1974), also by Raymond E. Mineck and Richard J. Margason (page images at HathiTrust)
• Langley Research Center: Pressure distribution on two models of a Project Mercury capsule for a mach number range of 1.60 to 6.01 and an angle-of-attack range of 0°degress to 180° (National Aeronautics and Space Administration, 1960), also by Robert A. Newlander, E. Brian Pritchard, and Nancy L. Taylor (page images at HathiTrust; US access only)
• Langley Research Center: Pressure distributions and aerodynamic characteristics of several spoiler controls on a 40 degree sweptback wing at a Mach number of 1.61 (National Aeronautics and Space Administration, 1960), also by Emma Jean Landrum and K. R. Czarnecki (page images at HathiTrust)
• Langley Research Center: Pressure distributions and shock shapes for 12.84/̊7 ̊on-axis and bent-nose biconics in air at mach 6 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Charles G. Miller, Peter A. Gnoffo, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Pressure distributions for a rectangular supersonic inlet at subsonic speeds (National Aeronautics and Space Administration ;, 1976), also by Dennis E. Fuller (page images at HathiTrust)
• Langley Research Center: Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by William G. Johnson and Acquilla S. Hill (page images at HathiTrust)
• Langley Research Center: Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by William G. Johnson, Otto Eichmann, and Acquilla S. Hill (page images at HathiTrust)
• Langley Research Center: Pressure distributions on 3 rigid wings simulating parawings with varied canopy curvature and leading-edge sweep at Mach numbers from 2.29 to 4.65 (National Aeronautics and Space Administration, 1963), also by Paul G. Fournier and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Pressure distributions on a rectangular aspect-ratio-6, slotted supercritical airfoil wing with externally blown flaps (U.S. National Aeronautics and Space Administration ;, 1976), also by William G. Johnson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Pressure gradient effects on heat transfer to reusable surface insulation tile-array gaps (National Aeronautics and Space Administration ;, 1975), also by David A. Throckmorton (page images at HathiTrust)
• Langley Research Center: Pressure measurements of the leading edge of a swept wing at Mach 2.2 (National Aeronautics and Space Administration ;, 1974), also by Russell B. Sorrells (page images at HathiTrust)
• Langley Research Center: Pressure measurements on a hypersonic glide configuration having 79.5 degree sweepback and 45 degree dihedral at a Mach number of 4.95 (National Aeronautics and Space Administration, 1959), also by Morton Cooper and Charles R. Gunn (page images at HathiTrust)
• Langley Research Center: Pressure measurements on a thick cambered and twisted 58 ̊delta wing at high subsonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Julio Chu and John E. Lamar (page images at HathiTrust)
• Langley Research Center: Pressure probe and hot-film probe responses to acoustic excitation in mean flow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Tony L. Parrott and Michael G. Jones (page images at HathiTrust)
• Langley Research Center: Principal results from wind-tunnel stability tests of several proposed space capsule models up to an angle of attack of 33 degree (National Aeronautics and Space Administration, 1959), also by Howard S. Carter, Roland D. English, and Ronald Kolenkiewicz (page images at HathiTrust)
• Langley Research Center: A Principled approach to the measurement of situation awareness in commercial aviation (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Yvette J. Tenney and BBN Systems and Technologies Corporation (page images at HathiTrust)
• Langley Research Center: Probability density functions in turbulent channel flow (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Surya P. G. Dinavahi and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: Probing the solar corona with spacecraft radio signals (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), also by Willard Wells, H. Hodara, R. Marquedant, and Inc Tetra Tech (page images at HathiTrust; US access only)
• Langley Research Center: A procedure for computing surface wave trajectories on an inhomogeneous surface (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Raymond L. Barger (page images at HathiTrust)
• Langley Research Center: A procedure for designing forebodies with constraints on cross-section shape and axial area distribution (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Raymond L. Barger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A procedure for estimating stability and control parameters from flight test data by using maximum likelihood methods employing a real-time digital system (National Aeronautics and Space Administration ;, 1972), also by Randall D. Grove (page images at HathiTrust)
• Langley Research Center: A procedure for rapid computation of equilibrium chemical composition and thermodynamic properties of the generalized argon-nitrogen-oxygen-hydrogen gas system (National Aeronautics and Space Administration ;, 1969), also by Vincent R. Mascitti and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Proceedings of NASA Conference on Supersonic-Transport Feasibility Studies and Supporting Research, September 17-19, 1963, Langley Research Center, Langley Station, Hampton, Va. Technical memorandum X-905. (National Aeronautics and Space Administration, 1963), also by Hampton NASA Conference on Supersonic-Transport Feasibility Studies and Supporting Research (1963 : Langley Research Center (page images at HathiTrust)
• Langley Research Center: Proceedings of the 1977 MACSYMA Users' Conference (Scientific and Technical Information Office, National Aeronautics and Space Administration ;, 1977), also by Calif.) MACSYMA Users' Conference (1977 : Berkeley, Berkeley University of California, and Massachusetts Institute of Technology (page images at HathiTrust)
• Langley Research Center: Processing of combined domestic bath and laundry waste waters for reuse as commode flushing water (National Aeronautics and Space Administration ;, 1975), also by Warren D. Hypes, Judd Rice Wilkins, and Carmen E. Batten (page images at HathiTrust)
• Langley Research Center: Products of some generalized functions (National Aeronautics and Space Administration ;, 1967), also by Robert C. Costen (page images at HathiTrust)
• Langley Research Center: Program and charts for determining shock tube, expansion tube, and expansion tunnel flow quantities for real air (National Aeronautics and Space Administration ;, 1975), also by Charles G. Miller and Sue E. Wilder (page images at HathiTrust)
• Langley Research Center: A program for calculating load coefficient matrices utilizing the force summation method, L218 (LOADS). (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by L. R. Anderson, R. D. Miller, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Program for determining aircraft equilibrium spin characteristics including stability. (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by William M. Adams (page images at HathiTrust)
• Langley Research Center: A program for equilibrium normal shock and stagnation point solutions for arbitrary gas mixtures (National Aeronautics and Space Administration ;, 1966), also by Linwood B. Callis and Jane T. Kemper (page images at HathiTrust)
• Langley Research Center: Program for rapid earth-to-space trajectory optimization (National Aeronautics and Space Administration ;, 1967), also by Richard C. Rosenbaum, Richard L. Moll, Robert E. Willwerth, Lockheed Missiles and Space Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Program for rendezvous mission trajectory optimization (National Aeronautics and Space Administration ;, 1967), also by Richard C. Rosenbaum, Richard L. Moll, Robert E. Willwerth, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A program to compute three-dimensional subsonic unsteady aerodynamic characteristics using the doublet lattice method, L216 (DUBFLEX) (National Aeronautics and Space Administration ;, 1979), also by M. Richard, B. A. Harrison, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Progress in aircraft design since 1903. (1974) (page images at HathiTrust)
• Langley Research Center: Project Fire Flight 1 vibration data (National Aeronautics and Space Administration ;, 1967), also by Herbert A. Leybold and Ling-Temco-Vought (page images at HathiTrust)
• Langley Research Center: Propeller aircraft interior noise model (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by L. D. Pope, John F. Wilby, E. G. Wilby, Beranek Bolt, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Properties of three graphite/toughened resin composites (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Donald L. Smith and Marvin B. Dow (page images at HathiTrust)
• Langley Research Center: Proposed technique for launching instrumented balloons into tornadoes. (National Aeronautics and Space Administration :, 1971), also by Frederick C. Grant and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Proton-radiation damage in Gunn oscillators (National Aeronautics and Space Administration ;, 1973), also by James W. Johnson and Carl L. Fales (page images at HathiTrust)
• Langley Research Center: Pseudosteady-state analysis of nonlinear aircraft maneuvers (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), also by John W. Young, Katherine G. Johnson, Albert A. Schy, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Psychophysical relationships characterizing human response to whole-body sinusoidal vertical vibration (National Aeronautics and Space Administration ;, 1976), also by Jack D. Leatherwood, Thomas K. Dempsey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Pulsed differential holographic measurements of vibration modes of high-temperature panels (National Aeronautics and Space Administration, 1972), also by D. A. Evensen, United States National Aeronautics and Space Administration, and TRW Systems Group (page images at HathiTrust)
• Langley Research Center: Q-circle measurement error (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Chase P. Hearn and Edward S. Bradshaw (page images at HathiTrust)
• Langley Research Center: Quantitative analysis of the reconstruction performance of interpolants (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Donald L. Lansing and Stephen Keith Park (page images at HathiTrust)
• Langley Research Center: Quantitative understanding of explosive stimulus transfer (National Aeronautics and Space Administration ;, 1973), also by M. L. Schimmel and McDonnell Aircraft Company (page images at HathiTrust)
• Langley Research Center: A quasi-omnidirectional slot array antenna for spacecraft use at microwave frequencies (National Aeronautics and Space Administration ;, 1968), also by W. F. Croswell, Douglas M. Hatcher, and C. M. Knop (page images at HathiTrust)
• Langley Research Center: R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Renaldo V. Jenkins (page images at HathiTrust)
• Langley Research Center: A radar test target system (National Aeronautics and Space Administration, 1960), also by James T. Rose and R. Donald Smith (page images at HathiTrust)
• Langley Research Center: Radiance of the earth and its limb in the middle ultraviolet (National Aeronautics and Space Administration, 1964), also by William C. Hrasky, Thomas B. McKee, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: Radiated noise from an externally blown flap (National Aeronautics and Space Administration ;, 1975), also by Narayana N. Reddy and James C. Yu (page images at HathiTrust)
• Langley Research Center: Radiation and scattering by thin-wire structures in the complex frequency domain (National Aeronautics and Space Administration ;, 1974), also by J. H. Richmond and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: Radiation exposure for manned Mars surface missions (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Lisa C. Simonsen (page images at HathiTrust)
• Langley Research Center: Radiation exposure in supersonic transports (National Aeronautics and Space Administration, 1962), also by Trutz Foelsche and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The radiation from apertures in curved surfaces (National Aeronautics and Space Administration ;, 1973), also by P. H. Pathak, R. G. Kouyoumjian, and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: The radiation from slots in truncated dielectric-covered surfaces (National Aeronautics and Space Administration ;, 1974), also by Y. M. Hwang, P. H. Pathak, R. G. Kouyoumjian, and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: Radiation measurements at supersonic transport altitude with balloon-borne nuclear emulsions (Pensacola, Florida : U.S. Naval Aerospace Medical Institute, U.S. Naval Aviation Medical Center, 1969., 1969), also by Hermann J. Schaefer, Naval Aerospace Medical Institute (U.S.), United States Navy Department Bureau of Medicine and Surgery, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Radiation protection for human missions to the moon and Mars (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Lisa C. Simonsen and John E. Nealy (page images at HathiTrust)
• Langley Research Center: Radiation risk predictions for Space Station Freedom orbits (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Francis A. Cucinotta (page images at HathiTrust)
• Langley Research Center: Radiative properties of advanced spacecraft heat shield materials (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by G. R. Cunnington, A. I. Funai, T. K. McNab, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Langley Research Center: Radiative property data for Venusian entry : a compendium (Scientific and Technical Information Office, Nation Aeronautics and Space Administration ;, 1974), also by Jim J. Jones (page images at HathiTrust)
• Langley Research Center: Radio blackout alleviation and plasma diagnostic results from a 25,000 foot per second blunt-body reentry (National Aeronautics and Space Administration ;, 1970), also by Norman D. Akey, Aubrey E. Cross, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Radio transmission through the plasma sheath around a lifting reentry vehicle (National Aeronautics and Space Administration :, 1961), also by Macon C. Ellis and Paul W. Huber (page images at HathiTrust)
• Langley Research Center: The radiometer transfer function for the AAFE composite two-frequency radiometer scatterometer (National Aeronautics and Space Administration ;, 1973), also by J. H. Moore and General Electric Company (page images at HathiTrust)
• Langley Research Center: Radiometric measurements of the earth's infrared horizon from the X-15 in three spectral intervals (National Aeronautics and Space Administration ;, 1968), also by Antony Jalink, Dwayne E. Hinton, Richard E. Davis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Radiometric observations of the earth's horizon from altitudes between 300 and 600 kilometers (National Aeronautics and Space Administration :, 1964), also by Thomas B. McKee, Charles D. Engle, and Ruth I. Whitman (page images at HathiTrust)
• Langley Research Center: A radionuclide counting technique for measuring wind velocity (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Jag J. Singh, Gerald H. Mall, G. S. Khandelwal, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Random-access technique for modular bathymetry data storage in a continental shelf wave refraction program (National Aeronautics and Space Administration ;, 1974), also by Lamont R. Poole (page images at HathiTrust)
• Langley Research Center: Random and systematic measurement errors in acoustic impedance as determined by the transmission line method (National Aeronautics and Space Administration ;, 1977), also by Tony L. Parrott, C. D. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Random harmonic analysis program, L221 (TEV156). (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by R. E. Clemmons, M. L. Graham, R. D. Miller, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Rapid estimation of frequency response functions by close-range photogrammetry (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by John S. Tripp (page images at HathiTrust)
• Langley Research Center: A rapid method for optimization of the rocket propulsion system for single-stage-to-orbit vehicles (National Aeronautics and Space Administration ;, 1976), also by Charles H. Eldred, Sabina V. Gordon, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Rapid methods for calculating radiation transport in the entry environment (National Aeronautics and Space Administration, 1975), also by William E. Nicolet and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A rapid numerical solution to subsonic flow over planar and axisymmetric profiles at an angle of attack of 0 ̊ (National Aeronautics and Space Administration ;, 1974), also by Vincent R. Mascitti (page images at HathiTrust)
• Langley Research Center: Rapid-transition tests of a 1/4-scale model of the VZ-2 tilt-wing aircraft (National Aeronautics and Space Administration, 1961), also by Louis P. Tosti and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Raster graphic helmet-mounted display study (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by William S. Beamon, Susanna I. Moran, United States. Army. Joint Research Programs Office, and General Electric Company. Simulation and Control Systems Dept (page images at HathiTrust)
• Langley Research Center: Reacting viscous-shock-layer solutions with multicomponent diffusion and mass injection (National Aeronautics and Space Administration ;, 1974), also by James N. Moss (page images at HathiTrust)
• Langley Research Center: Real-gas effects associated with one-dimensional transonic flow of cryogenic nitrogen (National Aeronautics and Space Administration ;, 1976), also by Jerry B. Adcock and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A real-time digital computer program for the simulation of automatic spacecraft reentries (National Aeronautics and Space Administration ;, 1977), also by Jack T. Kaylor, Richard W. Powell, Lawrence F. Rowell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Real-time processing of radar return on a parallel computer (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by David D. Aalfs and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: A real-time space station dynamics and control system simulation. (National Aeronautics and Space Administration :, 1971), also by Carolyn Grantham and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Realizable optimal control for a remotely piloted research vehicle (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by H. J. Dunn and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Realtime multi-plot graphics system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Michael S. Shipkowski and Wyle Laboratories (page images at HathiTrust)
• Langley Research Center: Recent advances in aerodynamic energy concept for flutter suppression and gust alleviation using active controls. (National Aeronautics and Space Administration ;, 1977), also by E. Nissim and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Recent advances in multidisciplinary analysis and optimization : proceedings of a symposium cosponsored by NASA Langley Research Center, NASA Lewis Research Center, and the Wright Research Development Center, and held in Hampton, Virginia, September 28-30, 1988 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989), also by Jean-Francois M. Barthelemy, Wright Research Development Center, Lewis Research Center, and Va.) NASA/Air Force Symposium on Recent Advances in Multidisciplinary Analysis and Optimization (2nd : 1988 : Hampton (page images at HathiTrust)
• Langley Research Center: Recent progress towards predicting aircraft ground handling performance (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Thomas J. Yager, Ellis J. White, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Recent research on V/STOL test limits at the University of Washington Aeronautical Laboratory (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Shojiro Shindo, William H. Rae, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: The receptivity of boundary layers on blunt bodies to oscillations in the free stream (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by C. E. Grosch and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Recirculation effects produced by a pair of heated jets impinging on a ground plane (National Aeronautics and Space Administration ;, 1969), also by Gordon R. Hall, Kenneth H. Rogers, Northrop Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Recommendations for field measurements of aircraft noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Alan H. Marsh and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Reconstruction of the 1st space shuttle (STS-1) entry trajectory (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), also by J. T. Findlay, G. M. Kelly, M. L. Heck, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Analytical Mechanics Associates (page images at HathiTrust)
• Langley Research Center: The red-shift-magnitude relation and observational data (National Aeronautics and Space Administration :, 1969), also by Windsor L. Sherman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Reduction method for thermal analysis of complex aerospace structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Charles P. Shore and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Reduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction (National Aeronautics and Space Administration ;, 1974), also by W. Pfenninger, J. Syberg, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Reduction of computer usage costs in predicting unsteady aerodynamicloadings caused by control surface motions : Analysis and results / W.S. Rowe, J.D. Sebastian, and J.R. Petrarca. (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by W. S. Rowe, J. R. Petrarca, J. D. Sebastian, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Reduction of high-speed impulsive noise by blade planform modification of a model helicopter rotor (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by David A. Conner, Danny R. Hoad, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Reference energy-altitude descent guidance : simulator evaluation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Kathy H. Abbott and Charles E. Knox (page images at HathiTrust)
• Langley Research Center: Reflection characteristics of artificial satellites constructed in the form of inflated polyhedrons (National Aeronautics and Space Administration, 1959), also by Archibald R. Sinclair (page images at HathiTrust)
• Langley Research Center: Refraction and scattering of sound by a shear layer (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Robert H. Schlinker, Roy K. Amiet, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Relative annoyance and loudness judgments of various simulated sonic boom waveforms (National Aeronautics and Space Administration ;, 1968), also by L. J. Shepherd, W. W. Sutherland, Stanford Research Institute, and Lockheed-California Company (page images at HathiTrust)
• Langley Research Center: Relative control effectiveness technique with application to airplane control coordination (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Frederick J. Lallman (page images at HathiTrust)
• Langley Research Center: Relative efficiency and accuracy of two Navier-Stokes codes for simulating attached transonic flow over wings (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Daryl L. Bonhaus and Stephen F. Wornom (page images at HathiTrust)
• Langley Research Center: Relative merits of reactive and forward-look detection for wind-shear encounters during landing approach for various microburst escape strategies (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by David A. Hinton (page images at HathiTrust)
• Langley Research Center: Relaxation of an unsteady turbulent boundary layer on a flat plate in an expansion tube (National Aeronautics and Space Administration ;, 1974), also by Roop N. Gupta and Robert L. Trimpi (page images at HathiTrust)
• Langley Research Center: Reliability bounds for fault-tolerant systems with competing responses to component failures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Larry D. Lee (page images at HathiTrust)
• Langley Research Center: Reliability of equivalent sphere model in blood-forming organ dose estimation (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Judy L. Shinn, John E. Nealy, and John W. Wilson (page images at HathiTrust)
• Langley Research Center: Reliability of laboratory tests of VSTOL and other long-duration noises (National Aeronautics and Space Administration ;, 1974), also by Karl D. Kryter and Stanford Research Institute (page images at HathiTrust)
• Langley Research Center: Reliable dual-redundant sensor failure detection and identification for the NASA F-8 DFBW aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by James C. Deckert and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Remote pilot-controlled docking with television (National Aeronautics and Space Administration ;, 1965), also by Edward R. Long, Perry L. Deal, and Jack E. Pennington (page images at HathiTrust)
• Langley Research Center: Remotely sensed and laboratory spectral signatures of an ocean-dumped acid waste (National Aeronautics and Space Administration ;, 1977), also by Beverly W. Lewis and Vernon G. Collins (page images at HathiTrust)
• Langley Research Center: Removal of spacecraft-surface particulate contaminants by simulated micrometeoroid impacts (National Aeronautics and Space Administration ;, 1974), also by J. H. Goad (page images at HathiTrust)
• Langley Research Center: A rendezvous and station-keeping simulator with fly-around capability and virtual-image viewing (National Aeronautics and Space Administration ;, 1969), also by William M. Kahlbaum, John J. Stumpf, Richard E. Bardusch, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Rendezvous capability of horizontal-take-off launch vehicle with air-breathing propulsion (National Aeronautics and Space Administration :, 1964), also by Charlie M. Jackson (page images at HathiTrust)
• Langley Research Center: Repair techniques for Celion/LARC-160 graphite/polyimide composite structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by J. S. Jones, Rockwell International, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and S.R. Graves (page images at HathiTrust)
• Langley Research Center: Requirements of a Martian television experiment for three point-mass descent trajectories (National Aeronautics and Space Administration ;, 1969), also by Friedrich O. Huck, Robert B. Spiers, Leonard P. Kopia, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Research and development program on cold cathode magnetron ultrahigh vacuum gage (National Aeronautics and Space Administration ;, 1969), also by Robert M. Oman and Norton Research Corporation (page images at HathiTrust)
• Langley Research Center: Research and development program on orbitron ultrahigh vacuum gauge (National Aeronautics and Space Administration ;, 1969), also by F. J. Brock and Norton Research Corporation (page images at HathiTrust)
• Langley Research Center: Research and technology 1987 : annual report of the Langley Research Center. (Langley Research Center, 1987) (page images at HathiTrust)
• Langley Research Center: Research and technology 1988 : annual report of the Langley Research Center. (Langley Research Center, 1988) (page images at HathiTrust)
• Langley Research Center: Research and technology 1990 (Langley Research Center ;, 1991) (page images at HathiTrust)
• Langley Research Center: Research and technology 1991 (Langley Research Center, 1991) (page images at HathiTrust)
• Langley Research Center: Research in aeronautics and space. (Langley Research Center, 1971) (page images at HathiTrust)
• Langley Research Center: Research in computerized structural analysis and synthesis : research-in-progress papers presented at a symposium cosponsored by NASA Langley Research Center and the George Washington University, in cooperation with the National Science Foundation and the American Society of Civil Engineers, and held at Washington, D.C., October 30 - November 1, 1978 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Harvey G. McComb, George Washington University, National Science Foundation (U.S.), American Society of Civil Engineers, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Research in digital adaptive flight controllers (U.S. National Aeronautics and Space Administration ;, 1976), also by Howard Kaufman, United States National Aeronautics and Space Administration, and Rensselaer Polytechnic Institute (page images at HathiTrust)
• Langley Research Center: Research in nonlinear structural and solid mechanics : keynote address and panel discussion presented at a symposium sponsored by NASA Langley Research Center, Hampton, Virginia, and the George Washington University, Washington, D.C., in cooperation with the National Science Foundation, the American Society of Civil Engineers, and the American Society of Mechanical Engineers, and held at Washington, D.C., October 6-8, 1980 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Harvey G. McComb, Ahmed Khairy Noor, and George Washington University (page images at HathiTrust)
• Langley Research Center: Research in nonlinear structural and solid mechanics : keynote address and panel discussion presented at a symposium (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Harvey G. McComb, Ahmed Khairy Noor, Joint Institute for Advancement of Flight Sciences, George Washington University, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and D.C.) Symposium on the Computational Methods in Nonlinear Structural and Solid Mechanics (1980 : Washington (page images at HathiTrust)
• Langley Research Center: Research in nonlinear structural and solid mechanics : research-in-progress papers presented at a symposium (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Harvey G. McComb, Ahmed Khairy Noor, American Society of Mechanical Engineers, American Society of Civil Engineers, Joint Institute for Advancement of Flight Sciences, George Washington University, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and D.C.) Symposium on the Computational Methods in Nonlinear Structural and Solid Mechanics (1980 : Washington (page images at HathiTrust)
• Langley Research Center: Research needs in heterogeneous tropospheric chemistry : proceedings of a workshop held in Sarasota, Florida January 9-13, 1984 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch and United States. Office of Space Science and Applications (page images at HathiTrust)
• Langley Research Center: Research on blunt-faced entry configurations at angles of attack Between 60° and 90° (National Aeronautics and Space Administration, 1960), also by William H. Phillips (page images at HathiTrust)
• Langley Research Center: Research study to provide concepts of panel attachment mechanisms suitable for refurbishable panel application (National Aeronautics and Space Administration ;, 1966), also by R. E. Rieckmann and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Residual strength and crack propagation tests on C-130 airplane center wings with service-imposed fatigue damage (National Aeronautics and Space Administration ;, 1972), also by H. Lawrence Snider, William Dirkin, Franklin L. Reeder, and Lockheed-Georgia Company (page images at HathiTrust)
• Langley Research Center: Residual strength of five boron/aluminum laminates with crack-like notches after fatigue loading (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by R. A. Simonds, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Langley Research Center: Response of a jet trainer aircraft to roughness of three runways (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information , Springfield, Virginia 20230], 1964), also by Garland J. Morris and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Response of a turbojet and a piston-engine transport airplane to runway roughness (National Aeronautics and Space Administration, 1965), also by Garland J. Morris and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Results from tests, with van-mounted sensor, of magnetic leader cable for aircraft guidance during roll-out and turnoff (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by James C. Young, Stewart H. Irwin, W. Thomas Bundick, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Results of aircraft open-loop tests of an experimental magnetic leader cable system for guidance during roll-out and turnoff (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by W. Thomas Bundick, William L. Poole, and David B. Middleton (page images at HathiTrust)
• Langley Research Center: Results of buffet tests in a cryogenic wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Richmond P. Boyden, William G. Johnson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Results of heating mode performance tests of a solar-assisted heat pump (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Clay B. Jones, Frederick O. Smetana, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Results of the examination of LDEF polyurethane thermal control coatings (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Johnny L. Golden (page images at HathiTrust)
• Langley Research Center: Results of the flight noise measurement program using a standard and modified SH-3A helicopter (National Aeronautics and Space Administration ;, 1973), also by Robert J. Pegg, David A. Hilton, Herbert R. Henderson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Results of the noise measurement program on a standard and modified OH-6A helicopter (National Aeronautics and Space Administration ;, 1973), also by Herbert R. Henderson, David A. Hilton, and Robert J. Pegg (page images at HathiTrust)
• Langley Research Center: Results of USAF-NASA-FAA Flight Program to study community responses to sonic booms in the Greater St. Louis area (National Aeronautics and Space Administration, 1965), also by Charles W. Nixon, Harvey H. Hubbard, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A Review and evaluation of the Langley Research Center's scientific and technical information program : results of phase VI--the technical report : a survey and analysis (National Aeronautics and Space Administration, Langley Research Center ;, 1982), also by Robert A. McCullough (page images at HathiTrust)
• Langley Research Center: A review of current procedures for normalizing aircraft flyover noise data to reference meteorological conditions (National Aeronautics and Space Administration ;, 1977), also by Richard DeLoach (page images at HathiTrust)
• Langley Research Center: Review of current status of prediction techniques (National Aeronautics and Space Administration ;, 1972), also by Richard E. Hayden and Beranek Bolt (page images at HathiTrust)
• Langley Research Center: A review of developments in the theory of elasto-plastic flow (National Aeronautics and Space Administration ;, 1973), also by J. L. Swedlow and Carnegie-Mellon University (page images at HathiTrust)
• Langley Research Center: Review of drag cleanup tests in Langley full-scale tunnel (from 1935 to 1945) applicable to current general aviation airplanes (National Aeronautics and Space Administration ;, 1976), also by Paul L. Coe and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A Review of flight and wind tunnel measurements of boundary layer pressure fluctuations and induced structural response (National Aeronautics and Space Administration ;, 1966), also by David Alan Bies and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A review of methodological factors in performance assessments of time-varying aircraft noise effects (National Aeronautics and Space Administration ;, 1977), also by Glynn D. Coates, Henry G. Luhring, Cephas J. Adkins, Earl A. Alluisi, and Old Dominion University (page images at HathiTrust)
• Langley Research Center: A Review of near-wall Reynolds-stress closures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Ronald M. C. So and Arizona State University. College of Engineering and Applied Sciences (page images at HathiTrust)
• Langley Research Center: Review of propulsion-induced effects on aerodynamics of jet/stol aircraft (National Aeronautics and Space Administration :, 1970), also by Richard J. Margason and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Review of sonic fatigue technology (National Aeronautics and Space Administration, Langley Research Center, 1994), also by B. L. Clarkson and Old Dominion University (page images at HathiTrust)
• Langley Research Center: Review of spectroscopic data for measurements of stratospheric species (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by James M. Hoell and Aaron Goldman (page images at HathiTrust)
• Langley Research Center: A Review of technologies applicable to low-speed flight of high-performance aircraft investigated in the Langley 14- by 22-foot subsonic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by John W. Paulson (page images at HathiTrust)
• Langley Research Center: A review of the NASA V-G/VGH General Aviation Program (National Aeronautics and Space Administration ;, 1975), also by Joseph W. Jewel and Garland J. Morris (page images at HathiTrust)
• Langley Research Center: A review of the theory of trailing edge noise (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by M. S. Howe and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Revised upper-air wind data for Wallops Island based on serially completed data for the years 1956 to 1964 (National Aeronautics and Space Administration, 1968), also by James A. Cochrane, William L. Weaver, Robert M. Henry, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: RF characteristics of the hoop column antenna for the land mobile satellite system mission (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Peter Foldes, Foldes Incorporated, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Rigid-body-control subsystem sizing for an earth science geostationary platform (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by A. Don Scott, Cheryl C. Jackson, and James A. Duricy (page images at HathiTrust)
• Langley Research Center: Ring-baffle pressure distribution and slosh damping in large cylindrical tanks (National Aeronautics and Space Administration ;, 1972), also by Harland F. Scholl, Phillip K. Davis, and David G. Stephens (page images at HathiTrust)
• Langley Research Center: Rocket exhaust ground cloud/atmospheric interactions (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by BaoChuan Hwang and Robert K. Gould (page images at HathiTrust)
• Langley Research Center: The Role of aerospace technology in agriculture : 1977 Summer Faculty Fellowship Program in Engineering Systems Design, NASA-Langley Research Center, American Society for Engineering Education, Old Dominion Research Foundation ([National Aeronautics and Space Administration] ;, 1977), also by Griffith John McRee, Old Dominion University. Research Foundation, American Society for Engineering Education, United States National Aeronautics and Space Administration, and Summer Faculty Fellowship Program in Engineering Systems Design (1977 : NASA Langley Research Center) (page images at HathiTrust)
• Langley Research Center: The Role of computers in research and development at Langley Research Center : proceedings of a workshop ... held at Langley Research Center, Hampton, Virginia, June 15-16, 1994 (National Aeronautics and Space Administration, 1994), also by Carol D. Wieseman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The role of fluctuating forces in the generation of compressor noise (National Aeronautics and Space Administration ;, 1972), also by Hanno H. Heller, Sheila E. Widnall, and Beranek Bolt (page images at HathiTrust)
• Langley Research Center: Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90/̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by William Mulcay, Julio Chu, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Rotary balance data for a single-engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 ̊to 90 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by William Mulcay, Robert A. Rose, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Rotary balance data for a single-engine trainer design for an angle-of-attack range of 8 ̊to 90/̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Paul Pantason, Waldo Dickens, Inc Bihrle Applied Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by William Bihrle, Robert Rose, William Mulcay, Randy S. Hultberg, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range 8 ̊to 90 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Randy S. Hultberg, William Bihrle, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 90.̊ II, High-wing model A (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by William Mulcay, Robert A. Rose, and Inc Bihrle Applied Research (page images at HathiTrust)
• Langley Research Center: Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 35.̊ III, Effect of wing leading-edge modifications model A (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by William Bihrle, William Mulcay, and Inc Bihrle Applied Research (page images at HathiTrust)
• Langley Research Center: Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8ê to 90ê. II, High-wing model C (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Randy S. Hultberg, Waldo Dickens, Julio Chu, and Inc Bihrle Applied Research (page images at HathiTrust)
• Langley Research Center: Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 90.̊ I, Low-wing model A (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Randy S. Hultberg, William Mulcay, and Inc Bihrle Applied Research (page images at HathiTrust)
• Langley Research Center: Rotary balance data for an F-15 model with fuel tanks for an angle-of-attack range of 8⁰ to 90⁰ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Billy Barnhart and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Rotational-temperature determination in flowing nitrogen using an electron beam (National Aeronautics and Space Administration, 1971), also by D. C. Lillicrap, L. P. Lee, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Rotorcraft blade mode damping identification from random responses using a recursive maximum likelihood algorithm (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by John A. Molusis, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Rough-air effect on crew performance during a simulated low-altitude high-speed surveillance mission (National Aeronautics and Space Administration, 1963), also by George J. Hurt (page images at HathiTrust)
• Langley Research Center: Rough-water ditching investigation of a model of a jet transport with the landing gear extended and with various ditching aids (National Aeronautics and Space Administration, 1959), also by William C. Thompson (page images at HathiTrust)
• Langley Research Center: Rule groupings : a software engineering approach towards verification of expert systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Mala Mehrotra and Inc ViGYAN (page images at HathiTrust)
• Langley Research Center: Salt-stress-corrosion cracking of residually stressed Ti-8Al-1Mo-1V brake-formed sheet at 550° F (561° K) (National Aeronautics and Space Administration ;, 1965), also by Richard A. Pride and John M. Woodard (page images at HathiTrust)
• Langley Research Center: Salt stress corrosion of residually stressed Ti-8Al-1Mo-1V alloy sheet after exposure at elevated temperatures (National Aeronautics and Space Administration ;, 1966), also by Howard B. Dexter (page images at HathiTrust)
• Langley Research Center: Saltation on Mars and expected lifetime of Viking 75 wind sensors (National Aeronautics and Space Administration ;, 1975), also by Robert M. Henry (page images at HathiTrust)
• Langley Research Center: Satellite measurements of tropospheric aerosols (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by M. Griggs and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A scaling technique for air-bearing simulation of precision pointing systems (National Aeronautics and Space Administration ;, 1971), also by Gordon F. Bullock, Frederick R. Morrell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A scanning laser-velocimeter technique for measuring two-dimensional wake-vortex velocity distributions (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Luther R. Gartrell, David B. Rhodes, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Scatter factor and reliability of aircraft structures (National Aeronautics and Space Administration ;, 1972), also by Gerhart I. Schuëller, Alfred Martin Freudenthal, and George Washington University (page images at HathiTrust)
• Langley Research Center: Science and technology of low speed and motorless flight : proceedings of a symposium cosponsored by NASA Langley Research Center and the Soaring Society of America, and held at NASA Langley Research Center, Hampton, Virginia, March 29-30, 1979 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Va.) International Symposium on the Science and Technology of Low Speed and Motorless Flight (3rd : 1979 : Hampton, Perry W. Hanson, and Soaring Society of America (page images at HathiTrust)
• Langley Research Center: Scientific and technical information output of the Langley Research Center for calendar year 1980 (NASA, 1981) (page images at HathiTrust)
• Langley Research Center: A search for residual magnetism along a tornado path (U.S. National Aeronautics and Space Administration, 1971), also by Robert C. Costen and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Second beamed space-power workshop : proceedings of a workshop sponsored by the National Aeronautics and Space Administration and held at NASA Langley Research Center Hampton, Virginia, February 28-March 2, 1989 (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989), also by R. J. De Young (page images at HathiTrust)
• Langley Research Center: Second International Symposium on Magnetic Suspension Technology : proceedings of a symposium sponsored by the National Aeronautics and Space Administration, Washington, D.C., and held in Seattle, Washington, August 11-13, 1993 (National Aeronautics and Space Administration ;, 1994), also by International Symposium on Magnetic Suspension Technology (2nd : 1993 : Langley Research Center), Colin P. Britcher, Nelson J. Groom, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A second-order accurate kinetic-theory-based method for inviscid compressible flows (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by S. M. Deshpande (page images at HathiTrust)
• Langley Research Center: A second order slender wing theory for wings with leading edge separation in supersonic flow (National Aeronautics and Space Administration :, 1971), also by Joseph P. Nenni, Chee Tung, United States National Aeronautics and Space Administration, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Langley Research Center: Second-order small-disturbance solutions for hypersonic flow over power-law bodies (National Aeronautics and Space Administration ;, 1975), also by James C. Townsend (page images at HathiTrust)
• Langley Research Center: Section data for thin, highly cambered airfoils in incompressible flow (National Aeronautics and Space Administration ;, 1971), also by Jerome H. Milgram, Massachusetts Institute of Technology, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Segmentation, dynamic storage, and variable loading on CDC equipment (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Sherwood H. Tiffany and Kentron International (page images at HathiTrust)
• Langley Research Center: Selected methods for quantification of community exposure to aircraft noise (U.S. National Aeronautics and Space Administration ;, 1976), also by Philip M. Edge and Jimmy M. Cawthorn (page images at HathiTrust)
• Langley Research Center: Selected NASA research in composite materials and structures. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Wash.) Industry Review of the NASA Aircraft Energy Efficiency Composite Programs (2nd : 1980 : Seattle and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Selected papers on environmental and attitude control of manned spacecraft (National Aeronautics and Space Administration ;, 1966) (page images at HathiTrust)
• Langley Research Center: Semianalytic modeling of aerodynamic shapes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Raymond L. Barger and Mary S. Adams (page images at HathiTrust)
• Langley Research Center: Semiconductor diode laser material and devices with emission in visible region of the spectrum (National Aeronautics and Space Administration ;, 1975), also by I. Ladany, Henry Kressel, and RCA Laboratories (page images at HathiTrust)
• Langley Research Center: A semiempirical collision model for plasmas (National Aeronautics and Space Administration ;, 1969), also by Willard E. Meador and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A semiempirical method for obtaining fuselage normal areas from fuselage Mach sliced areas (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Robert J. Mack and Kathy E. Needleman (page images at HathiTrust)
• Langley Research Center: Semiempirical method for predicting effects of incident-reflecting shocks on the turbulent boundary layer (National Aeronautics and Space Administration ;, 1965), also by S. Z. Pinckney (page images at HathiTrust)
• Langley Research Center: Sensitivity analysis of torsional vibration characteristics of helicopter rotor blades (National Aeronautics and Space Administration ;, 1974), also by Theodore Bratanow, Akin Ecer, and University of Wisconsin--Milwaukee (page images at HathiTrust)
• Langley Research Center: Sensitivity of short-period tracking data from a lunar satellite to the lunar gravitational field harmonics (National Aeronautics and Space Administration ;, 1965), also by William R. Wells (page images at HathiTrust)
• Langley Research Center: Sensitivity of space shuttle weight and cost to structure subsystem weights (National Aeronautics and Space Administration ;, 1973), also by T. E. Wedge, R. P. Williamson, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Langley Research Center: Separated flow over bodies of revolution using an unsteady discrete-vorticity cross wake. Part 2, Computer program description (National Aeronautics and Space Administration ;, 1974), also by F. J. Marshall, F. D. Deffenbaugh, and Purdue University. School of Aeronautics and Astronautics (page images at HathiTrust)
• Langley Research Center: Service evaluation of aluminum brazed titanium (ABTi) (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by S. D. Elrod and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Service evaluation of aluminum brazed titanium (ABTi) jet engine tailpipe extensions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by S. D. Elrod and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Shape sensitivity analysis of wing static aeroelastic characteristics (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Jean-Francois M. Barthelemy and Fred D. Bergen (page images at HathiTrust)
• Langley Research Center: Shear-flexible finite-element models of laminated composite plates and shells (National Aeronautics and Space Administration ;, 1975), also by Ahmed Khairy Noor and Michael D. Mathers (page images at HathiTrust)
• Langley Research Center: Shear-lag analysis of a hybrid, unidirectional composite with fiber damage (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by J. G. Goree, Lokeswarappa R. Dharani, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Shear-lag analysis of notched laminates with interlaminar debonding (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), also by J. G. Goree, Autar K. Kaw, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Clemson University (page images at HathiTrust)
• Langley Research Center: Shear-stress intensity factors for elastic sheets with cover plates (National Aeronautics and Space Administration ;, 1974), also by W. B. Fichter (page images at HathiTrust)
• Langley Research Center: Shearing of a corrugated plate with curvilinear corrugations (National Aeronautics and Space Administration ;, 1972), also by Lung-Hsiang Wu, Charles Libove, and Syracuse University (page images at HathiTrust)
• Langley Research Center: Shock associated noise reduction from inverted-velcoity-profile coannular jets (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1981), also by H. K. Tanna, W. H. Brown, C. K. W. Tam, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: The shock expansion tube and its application as a sonic boom simulator (National Aeronautics and Space Administration, 1968), also by Hugo E. Dahlke, LTV Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Shock interference heat transfer to tank configurations mated to a straight-wing space shuttle orbiter at mach number 10.3 (National Aeronautics and Space Administration ;, 1976), also by Davis H. Crawford and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Shock shapes on blunt bodies in hypersonic-hypervelocity helium, air, and CO₂ flows, and calibration results in Langley 6-inch expansion tube (National Aeronautics and Space Administration ;, 1975), also by Charles G. Miller (page images at HathiTrust)
• Langley Research Center: Shock-tube heat-transfer measurements on inner surface of a cylinder (simulating a flat plate) for stagnation-temperature range 4,100 ̊to 8,300 ̊R (National Aeronautics and Space Administration, 1959), also by Jim J. Jones (page images at HathiTrust)
• Langley Research Center: Shock-tube study of the reaction H + O₂ + Ar [rightward-pointing arrow] HO₂ + Ar (National Aeronautics and Space Administration ;, 1972), also by Casimir J. Jachimowski and William M. Houghton (page images at HathiTrust)
• Langley Research Center: Shock wave interaction with an abrupt area change (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Manuel D. Salas (page images at HathiTrust)
• Langley Research Center: A short static-pressure probe design for supersonic flow (National Aeronautics and Space Administration ;, 1975), also by S. Z. Pinckney (page images at HathiTrust)
• Langley Research Center: Should helicopter noise be measured differently from other aircraft noise? : a review of the psychoacoustic literature (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by John A. Molino, Wyle Laboratories, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 (National Aeronautics and Space Administration, 1959), also by Gerald V. Foster (page images at HathiTrust)
• Langley Research Center: Sidewall boundary-layer measurements with upstream suction in the Langley 0.3-meter Transonic Cryogenic Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by A. V. Murthy (page images at HathiTrust)
• Langley Research Center: Signal-to-noise ratio analysis and evaluation of the Hadamard imaging technique (National Aeronautics and Space Administration ;, 1977), also by Daniel J. Jobson, Robert B. Spiers, and S. J. Katzberg (page images at HathiTrust)
• Langley Research Center: Similitude requirements and scaling relationships as applied to model testing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Chester H. Wolowicz, William P. Gilbert, James S. Bowman, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A simple method for converting frequency-domain aerodynamics to the time domain (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by E. H. Dowell (page images at HathiTrust)
• Langley Research Center: Simple method of using onboard optical measurements to predict the orbit established after the lunar-ascent-transfer orbit (National Aeronautics and Space Administration ;, 1970), also by L. Keith Barker and Herman S. Fletcher (page images at HathiTrust)
• Langley Research Center: A simplified approach to axisymmetric dual-reflector antenna design (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Raymond L. Barger (page images at HathiTrust)
• Langley Research Center: A simplified fourwall interference assessment procedure for airfoil data obtained in the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987), also by A. V. Murthy (page images at HathiTrust)
• Langley Research Center: Simplified free-energy calculation for ion-induced heteromolecular nucleation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Jag J. Singh, Institute for Atmospheric Optics & Remote Sensing, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A simplified holographic-interferometry technique for real-time flow visualization and analysis (National Aeronautics and Space Administration ;, 1974), also by Sheila Ann T. Long, Don M. Robinson, and Robert C. Spencer (page images at HathiTrust)
• Langley Research Center: Simplified interplanetary guidance procedures using onboard optical measurements (National Aeronautics and Space Administration ;, 1972), also by Harold A. Hamer and Katherine G. Johnson (page images at HathiTrust)
• Langley Research Center: A simplified method for determining heat of combustion of natural gas (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Jag J. Singh, Gerald H. Mall, and Hoshang Chegini (page images at HathiTrust)
• Langley Research Center: A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by David M. McGowan, Stephen J. Scotti, and Charles J. Camarda (page images at HathiTrust)
• Langley Research Center: Simplified model for solar cosmic ray exposure in manned earth orbital flights (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by John W. Wilson (page images at HathiTrust)
• Langley Research Center: A simplified model for the viscous crossflow in a slotted test section (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Charlie H. Cooke and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Simulaion of ideal-gas flow by nitrogen and other selected gases at cyogenic temperatures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Robert M. Hall, Jerry B. Adcock, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Simulated-airline-service flight tests of laminar flow control with perforated-surface suction system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Dal V. Maddalon and Albert L. Braslow (page images at HathiTrust)
• Langley Research Center: Simulated indoor sonic booms judged relative to noise from subsonic aircraft (National Aeronautics and Space Administration ;, 1972), also by Karl D. Kryter, Jerome S. Lukas, and Stanford Research Institute (page images at HathiTrust)
• Langley Research Center: Simulation and flight evaluation of a head-up landing aid for general aviation (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Randall L. Harris, Kenneth R. Yenni, Maxwell W. Goode, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Simulation comparison of a decoupled longitudinal control system and a velocity-vector control wheel steering system during landings in wind shear (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by G. Kimball Miller and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A simulation evaluation of a pilot interface with an automatic terminal approach system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by David A. Hinton (page images at HathiTrust)
• Langley Research Center: A simulation evaluation of the Engine Monitoring and Control System display (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Terence S. Abbott (page images at HathiTrust)
• Langley Research Center: A simulation investigation of the loads experienced by a piloted launch vehicle (National Aeronautics and Space Administration ;, 1966), also by Robert K. Sleeper (page images at HathiTrust)
• Langley Research Center: Simulation of a hydrocarbon fueled scramjet exhaust (National Aeronautical and Space Administration, Scientific and Technical Information Branch ;, 1982), also by J. Leng, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Simulation of decelerating landing approaches on an externally blown flap STOL transport airplane (National Aeronautics and Space Administration ;, 1974), also by William D. Grantham, Perry L. Deal, and Luat T. Nguyen (page images at HathiTrust)
• Langley Research Center: Simulation of flight test conditions in the Langley pilot transonic cryogenic tunnel (National Aeronautics and Space Administration ;, 1974), also by Robert A. Kilgore, Edward J. Ray, and Jerry B. Adcock (page images at HathiTrust)
• Langley Research Center: Simulation of hypersonic scramjet exhaust (National Aeronautics and Space Administration ;, 1975), also by R. A. Oman and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Simulation of pyrolysis-gas flow through a char layer during ablation (National Aeronautics and Space Administration ;, 1969), also by Ronald K. Clark (page images at HathiTrust)
• Langley Research Center: Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by John R. Micol (page images at HathiTrust)
• Langley Research Center: Simulation of turbulent wall pressure (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Robert L. Ash and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Simulation studies of some supersonic transport instrumentation requirements and operating problems (National Aeronautics and Space Administration, 1969), also by Norman S. Silsby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Simulation studies of STOL airplane operations in metropolitan downtown and airport air traffic control environments (National Aeronautics and Space Administration ;, 1974), also by Richard H. Sawyer and Milton D. McLaughlin (page images at HathiTrust)
• Langley Research Center: Simulation studies of the supersonic transport in future air traffic control systems (National Aeronautics and Space Administration ;, 1968), also by Richard H. Sawyer, Milton D. McLaughlin, and Norman S. Silsby (page images at HathiTrust)
• Langley Research Center: Simulation study of a geometric shape factor technique for estimating earth-emitted radiant flux densities from wide-field-of-view radiation measurements (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by William L. Weaver, Richard N. Green, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A simulation study of curved, descending, decelerating, landing approaches for transport aircraft (U.S. National Aeronautics snd Space Administration, Langley Research Center, 1976), also by James E. Dieudonne, Randall D. Grove, and George G. Steinmetz (page images at HathiTrust)
• Langley Research Center: Simulation study of intracity helicopter operations under instrument conditions to category I minimums (National Aeronautics and Space Administration ;, 1974), also by William M. Callan, Daniel J. DiCarlo, and Jacob A. Houck (page images at HathiTrust)
• Langley Research Center: A simulation study of the flight dynamics of elastic aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987), also by Martin R. Waszak, D. K. Schmidt, and John B. Davidson (page images at HathiTrust)
• Langley Research Center: Simulator evaluation of separation of display parameters in path-following tasks (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Garimella R. Sarma, James J. Adams, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Simulator evaluation of the effects of reduced spoiler and thrust authority on a decoupled longitudinal control system during landings in wind shear (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by G. Kimball Miller and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A simulator evaluation of the use of spoilers on a light aircraft (National Aeronautics and Space Administration ;, 1972), also by Carl H. Brainerd, David L. Kohlman, and University of Kansas. Center for Research (page images at HathiTrust)
• Langley Research Center: A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by William D. Grantham, Perry L. Deal, Paul M. Smith, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Simulator study of a pictorial display for general aviation instrument flight (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by James J. Adams and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A simulator study of a pictorial navigation display in instrument departures of the supersonic transport (National Aeronautics and Space Administration, 1967), also by Norman W. Silsby, Michael C. Fischer, and United States. National Aeronautics and Space Center (page images at HathiTrust)
• Langley Research Center: Simulator study of ability of pilots to establish near-circular lunar orbits using simplified guidance techniques (National Aeronautics and Space Administration :, 1965), also by G. Kimball Miller and Herman S. Fletcher (page images at HathiTrust)
• Langley Research Center: Simulator study of flight characteristics of several large dissimilar, cargo transport airplanes during approach and landing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by William D. Grantham (page images at HathiTrust)
• Langley Research Center: Simulator study of minimum acceptable level of longitudinal stability for a representative STOL configuration during landing approach (National Aeronautics and Space Administration ;, 1974), also by William D. Grantham and Perry L. Deal (page images at HathiTrust)
• Langley Research Center: A simulator study of pilot control of remote orbital docking of large attitude-stabilized components (National Aeronautics and Space Administration ;, 1967), also by Donald R. Riley and William T. Suit (page images at HathiTrust)
• Langley Research Center: Simulator study of stall/post-stall characteristics of a fighter airplane with longitudinal static stability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Luat T. Nguyen and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A simulator study of the control of lunar flying platforms by pilot body motions (National Aeronautics and Space Administration, 1970), also by Paul R. Hill, David F. Thomas, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Simulator study of the effect of visual-motion time delays on pilot tracking performance with an audio side task (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Donald R. Riley, G. Kimball Miller, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A simulator study of the effectiveness of a pilot's indicator which combined angle of attack and rate of change of total pressure as applied to the take-off rotation and climbout of a supersonic transport (National Aeronautics and Space Administration, 1961), also by Albert W. Hall, Jack E. Harris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Simulator study of the stall departure characteristics of a light general aviation airplane with and without a wing-leading-edge modification (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Donald R. Riley (page images at HathiTrust)
• Langley Research Center: Simulator study of vortex encounters by a twin-engine, commercial, jet transport airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Earl C. Hastings, Gerald L. Keyser, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Single Bridgewire Apollo Standard Initiator (National Aeronautics and Space Administration ;, 1975), also by S. J. Salter, G. L. McDougal, R. E. Lundberg, and MB Associates (page images at HathiTrust)
• Langley Research Center: Single launch lunar habitat derived from NSTS external tank (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Charles B. King (page images at HathiTrust)
• Langley Research Center: Single-mode laser studies : (I) design and performance of a fixed-wavelength laser source and (II) coupling of lasers to thin-film optical waveguides (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by I. Ladany, J. M. Hammer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Single pilot IFR accident data analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by D. F. Harris, J. A. Morrisette, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Spectrum Technology Incorporated (page images at HathiTrust)
• Langley Research Center: Singular extremaloids in optimal control theory and the calculus of variations (National Aeronautics and Space Administration ;, 1970), also by Terry A. Straeter and North Carolina State University (page images at HathiTrust)
• Langley Research Center: Singular perturbation techniques for real time aircraft trajectory optimization and control (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Anthony J. Calise, Daniel D. Moerder, Drexel University. Dept. of Mechanical Engineering & Mechanics, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Sinusoidal reaction formulation for radiation and scattering from conducting surfaces (National Aeronautics and Space Administration ;, 1974), also by J. H. Richmond, N. Wang, and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: Site selection and directional models of deserts used for ERBE validation targets (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by W. Frank Staylor (page images at HathiTrust)
• Langley Research Center: Six-inch subsonic high-temperature arc tunnel for structures and material tests (National Aeronautics and Space Administration, 1963), also by Ronald D. Brown, L. Ross Levin, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Skin friction reduction by slot injection at mach 0.8 (U.S. National Aeronautics and Space Administration ;, 1976), also by Victor Zakkay, Chi R. Wang, United States National Aeronautics and Space Administration, and New York University (page images at HathiTrust)
• Langley Research Center: Skin friction reduction in supersonic flow by injection through slots, porous sections and combinations of the two (National Aeronautics and Space Administration ;, 1975), also by Joseph A. Schetz, Johannes VanOvereem, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Langley Research Center: Slip-boundary equations for multicomponent nonequilibrium airflow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Roop N. Gupta, James N. Moss, and Carl D. Scott (page images at HathiTrust)
• Langley Research Center: Slope diffraction analysis of tem parallel-plate patterns (National Aeronautics and Space Administration ;, 1969), also by D. C. F. Wu, R. C. Rudduck, and Ohio State University (page images at HathiTrust)
• Langley Research Center: A small gas inlet system for orbital mass-spectrometer calibrations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Alphonsa Smith, Richard E. Stell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A small multi-purpose rocket payload for ionospheric studies (National Aeronautics and Space Administration, 1964), also by S. J. Bauer, J. E. Jackson, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: Small plasma probes with guard rings and thermocouples (National Aeronautics and Space Administration ;, 1966), also by James F. Morris (page images at HathiTrust)
• Langley Research Center: A small volume, ultrahigh vacuum system for ionization gage studies (National Aeronautics and Space Administration ;, 1967), also by R. A. Outlaw and James M. Bradford (page images at HathiTrust)
• Langley Research Center: The smoke-trail method for obtaining detailed measurements of the vertical wind profile for application to missile-dynamic-response problems (National Aeronautics and Space Administration, 1961), also by Robert M. Henry and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Software design for automated assembly of truss structures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Catherine L. Herstrom (page images at HathiTrust)
• Langley Research Center: Software reuse issues : proceedings of a workshop (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Kathryn A. Smith and Susan J. Voigt (page images at HathiTrust)
• Langley Research Center: Solar assisted heat pumps : a possible wave of the future. (National Aeronautics and Space Administration ;, 1976), also by Frederick O. Smetana, North Carolina Science and Technology Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Solid Rocket Motor Witness Test (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Christopher S. Welch and College of William and Mary. Dept. of Physics (page images at HathiTrust)
• Langley Research Center: Solution of axisymmetric and two-dimensional inviscid flow over blunt bodies by the method of lines (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by H. Harris Hamilton and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Solution of complex nonlinear problems by a generalized application of the method of base and comparison solutions with applications to aerodynamics problems (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Raymond L. Barger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Solution of the exact equations for three-dimensional atmospheric entry using directly matched asymptotic expansions (U.S. National Aeronautics and Space Administration, Langley Research Center ;, 1976), also by Adolf Busemann, Robert D. Culp, Nguyen X. Vinh, and University of Colorado (page images at HathiTrust)
• Langley Research Center: Solutions of blunt-body stagnation-region flows with nongray emission and absorption of radiation by a time-asymptotic technique (National Aeronautics and Space Administration ;, 1969), also by Linwood B. Callis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Some aerodynamic and control studies of lifting reentry configurations at angles of attack up to 90° at a mach number of 2.91 (National Aeronautics and Space Administration, 1960), also by Frank L. Clark and Joanna M. Evans (page images at HathiTrust; US access only)
• Langley Research Center: Some analyses of the variability of atmospheric parameters at low altitudes significant for aircraft propagation (National Aeronautics and Space Administration, 1972), also by David T. Chang, United States National Aeronautics and Space Administration, and Allied Research Associates (page images at HathiTrust)
• Langley Research Center: Some anomalies observed in wind-tunnel tests of a blunt body at transonic and supersonic speeds (National Aeronautics and Space Administration ;, 1976), also by Joseph D. Brooks and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Some aspects of air-helium simulation and hypersonic approximations (National Aeronautics and Space Administration, 1959), also by Eugene S. Love, Mitchel H. Bertram, and Arthur Henderson (page images at HathiTrust)
• Langley Research Center: Some aspects of essentially nonoscillatory (ENO) formulations for the Euler equations (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Sukumar R. Chakravarthy and Rockwell International. Science Center (page images at HathiTrust)
• Langley Research Center: Some aspects of optical feedback with cadmium sulfide and related photoconductors (National Aeronautics and Space Administration ;, 1974), also by S. J. Katzberg (page images at HathiTrust)
• Langley Research Center: Some cable suspension systems and their effects on the flexural frequencies of slender aerospace structures (National Aeronautics and Space Administration ;, 1974), also by Robert W. Herr (page images at HathiTrust)
• Langley Research Center: Some effects of adverse weather conditions on performance of airplane antiskid braking systems (National Aeronautics and Space Administration ;, 1976), also by Walter B. Horne, John A. Tanner, John L. McCarty, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Some effects of control profile and control trailing-edge angle on the oscillating hinge-moment and flutter characteristics of flap-type controls at transonic speeds (National Aeronautics and Space Administration, 1960), also by William C. Moseley, Thomas G. Gainer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Some effects of flight path and atmospheric variations on the boom propagated from a supersonic aircraft (National Aeronautics and Space Administration, 1964), also by Raymond L. Barger and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Some effects of grooved runway configurations on aircraft tire braking traction under flooded runway conditions (National Aeronautics and Space Administration ;, 1973), also by Thomas A. Byrdsong and Thomas J. Yager (page images at HathiTrust)
• Langley Research Center: Some effects of tip fins of wing flutter characteristics (National Aeronautics and Space Administration ;, 1974), also by Robert C. Goetz and Robert V. Doggett (page images at HathiTrust)
• Langley Research Center: Some experiments concerning subsequent yield surfaces in plasticity (National Aeronautics and Space Administration, 1960), also by Harvey G. McComb (page images at HathiTrust)
• Langley Research Center: Some factors affecting the stress-corrosion cracking of Ti-6Al-4V alloy in methanol (National Aeronautics and Space Administration ;, 1969), also by W. Barry Lisagor and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Some landing studies pertinent to glider-reentry vehicles (National Aeronautics and Space Administration :, 1960), also by John C. Houbolt and Sidney A. Batterson (page images at HathiTrust)
• Langley Research Center: Some loading conditions imposed by ground turning maneuvers with three jet transport airplanes (NASA ;, 1972), also by Albert W. Hall and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Some nonasymptotic effects on the sonic boom of large airplanes (National Aeronautics and Space Administration, 1965), also by F. Edward McLean and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Some notes on attitude control of earth satellite vehicles (National Aeronautics and Space Administration, 1959), also by Warren Gillespie, Allan B. Churgin, and Donald G. Eide (page images at HathiTrust)
• Langley Research Center: Some observations during weightlessness simulation with subject immersed in a rotating water tank (National Aeronautics and Space Administration :, 1964), also by Ralph W. Stone and William Letko (page images at HathiTrust)
• Langley Research Center: Some observations on a new numerical method for solving the Navier-Stokes equations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Ajay Kumar and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Some path-following techniques for solution of nonlinear equations and comparison with parametric differentiation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Raymond L. Barger and Robert W. Walters (page images at HathiTrust)
• Langley Research Center: Some problems of the calculation of three-dimensional boundary-layer flows on general configurations (National Aeronautics and Space Administration ;, 1973), also by Tuncer Cebeci and Douglas Aircraft Company (page images at HathiTrust)
• Langley Research Center: Some recent developments in the prediction of shock interaction phenomena at hypersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Davis H. Crawford and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Some remarks on the design of transonic tunnels with low levels of flow unsteadiness (National Aeronautics and Space Administration ;, 1976), also by Dennis G. Mabey and Royal Aircraft Establishment (Great Britain). Structures Dept (page images at HathiTrust)
• Langley Research Center: Sonic-boom characteristics in the extreme near field of a complex airplane model at mach numbers of 1.5, 1.8, and 2.5 (National Aeronautics and Space Administration, 1970), also by Odell A. Morris, Harry W. Carlson, Milton Lamb, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Sonic-boom characteristics of proposed supersonic and hypersonic airplanes (National Aeronautics and Space Administration, 1966), also by F. Edward McLean, Lynn W. Hunton, Harry W. Carlson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Sonic-boom ground-pressure measurements from Apollo 15 (National Aeronautics and Space Administration ;, 1972), also by David A. Hilton, Royce L. McKinney, and Herbert R. Henderson (page images at HathiTrust)
• Langley Research Center: Sonic-boom ground pressure measurements from the launch and reentry of Apollo 16 (National Aeronautics and Space Administration ;, 1974), also by Herbert R. Henderson and David A. Hilton (page images at HathiTrust)
• Langley Research Center: Sonic boom in turbulence (National Aeronautics and Space Administration ;, 1971), also by W. A. Horning, United States National Aeronautics and Space Administration, and inc EG & G (page images at HathiTrust)
• Langley Research Center: Sonic-boom measurements during bomber training operations in the Chicago area (National Aeronautics and Space Administration, 1966), also by David A. Hilton, Domenic J. Maglieri, Vera Huckel, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Sonic-boom measurements in the focus region during the ascent of Apollo 17 (National Aeronautics and Space Administration ;, 1974), also by Herbert R. Henderson and David A. Hilton (page images at HathiTrust)
• Langley Research Center: Sonic-boom minimization with nose-bluntness relaxation (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Christine M. Darden and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Sonic boom propagation in a stratified atmosphere, with computer program (National Aeronautics and Space Administration, 1969), also by Wallace D. Hayes, H. E. Kulsrud, Rudolph C. Haefeli, United States National Aeronautics and Space Administration, and Inc Aeronautical Research Associates of Princeton (page images at HathiTrust)
• Langley Research Center: Sonic-boom wave-front shapes and curvatures associated with maneuvering flight (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Raymond L. Barger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Sonic booms from aircraft in maneuvers (National Aeronautics and Space Administration, 1964), also by Domenic J. Maglieri, Donald L. Lansing, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Sound scattering by rigid oblate spheroids, with implication to pressure gradient microphones (U.S. National Aeronautics and Space Administration ;, 1976), also by Algirdas Maciulaitis, Thomas D. Norum, John M. Seiner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Sound speed measurements in liquid oxygen-liquid nitrogen mixtures (NASA Langley Research Center [For sale by the National Technical Information Service], 1985), also by Allan J. Zuckerwar (page images at HathiTrust)
• Langley Research Center: Source mechanisms for rotor noise radiation (National Aeronautics and Space Administration ;, 1973), also by M. V. Lowson, C. E. Whitfield, A. R. Whatmore, and Loughborough University of Technology (page images at HathiTrust)
• Langley Research Center: Sources, control, and effects of noise from aircraft propellers and rotors (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John S. Mixson, Thomas K. Dempsey, and George C. Greene (page images at HathiTrust)
• Langley Research Center: Space environmental effects on spacecraft : LEO materials selection guide (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by Edward M. Silverman and TRW Inc. Space & Electronics Group (page images at HathiTrust)
• Langley Research Center: Space radiation dose analysis for solar flare of August 1989 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by John E. Nealy (page images at HathiTrust)
• Langley Research Center: Space shuttle orbiter trimmed center-of-gravity extension study : summary report (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by William I. Scallion and W. Pelham Phillips (page images at HathiTrust)
• Langley Research Center: Space shuttle phase B wind tunnel test database : summary report (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by J. L. Glynn and D. E. Poucher (page images at HathiTrust)
• Langley Research Center: Space station crew safety alternatives study : final report (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985), also by R. L. Peercy (page images at HathiTrust)
• Langley Research Center: Span loadings and aerodynamic characteristics for a series of tip and trailing-edge controls on a 60 degree delta wing at Mach numbers of 1.61 and 2.01 (National Aeronautics and Space Administration, 1959), also by K. R. Czarnecki and Douglas R. Lord (page images at HathiTrust)
• Langley Research Center: Span reduction effects on flutter characteristics of arrow-wing supersonic transport configurations (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Donald F. Keller and Ellen Parker Bullock (page images at HathiTrust)
• Langley Research Center: Spanwise loadings and aerodynamic characteristics for a series of trailing-edge controls on a 40 degree sweptback wing at Mach numbers of 1.61 and 2.01 (National Aeronautics and Space Administration, 1962), also by Emma Jean Landrum and K. R. Czarnecki (page images at HathiTrust)
• Langley Research Center: Spanwise measurements of vertical components of atmospheric turbulence (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Robert K. Sleeper (page images at HathiTrust)
• Langley Research Center: Sparse matrix methods research using the CSM Testbed software system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Eleanor Chin-hwa Chu and J. Alan George (page images at HathiTrust)
• Langley Research Center: Spatial frequency response of an optical heterodyne receiver (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), also by Don M. Robinson, Carl L. Fales, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Spatial-frequency response of the limb infrared monitor of the stratosphere (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by R. Gale Wilson, William M. Kahlbaum, Antony Jalink, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Spectral properties of gaseous Uranium Hexafluoride at high temperature (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1980), also by N. L. Krascella and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A spectrographic analysis of a 1-foot hypersonic-arc-tunnel airstream using an electron beam probe (National Aeronautics and Space Administration, 1964), also by Daniel I. Sebacher, Roy J. Duckett, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Spectrographic temperature measurements in a carbon-arc-powered air jet (National Aeronautics and Space Administration, 1959), also by David H. Greenshields (page images at HathiTrust)
• Langley Research Center: Spectrometric measurements of gas temperatures in arc-heated jets and tunnels (National Aeronautics and Space Administration, 1963), also by David H. Greenshields (page images at HathiTrust)
• Langley Research Center: Spectrophotometer-integrating-sphere system for computing solar absorptance (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by William G. Witte, John E. Perry, and Wayne S. Slemp (page images at HathiTrust)
• Langley Research Center: Spectroscopic analysis of radiation-generated changes in tensile properties of a polyetherimide film (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Edward R. Long and Sheila Ann T. Long (page images at HathiTrust)
• Langley Research Center: Spectroscopic comparison of effects of electron radiation on mechanical properties of two polyimides (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Edward R. Long and Sheila Ann T. Long (page images at HathiTrust)
• Langley Research Center: Spin dynamics of manned space stations (National Aeronautics and Space Administration :, 1963), also by Peter R. Kurzhals, Claude R. Keckler, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Spin dynamics of manned space stations (Langley Research Center, 1963), also by Peter R. Kurzhals, Claude R. Keckler, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A spin-recovery parachute system for light general-aviation airplanes (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Charles F. Bradshaw and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: The spin-temperature theory of dynamic nuclear polarization and nuclear spin-lattice relaxation (National Aeronautics and Space Administration ;, 1974), also by Charles E. Byvik and David S. Wollan (page images at HathiTrust)
• Langley Research Center: Spin tests of a single-engine, high-wing light airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Eric C. Stewart and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Spin-tunnel investigation of a 1/13-scale model of the NASA AD-1 oblique-wing research aircraft (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by William L. White, James S. Bowman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Spline methods for approximating quantile functions and generating random samples (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by James R. Schiess, Christine G. Matthews, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Stability analysis for laminar flow control. (National Aeronautics and Space Administration ;, 1977), also by David J. Benney, Steven A. Orszag, and inc Cambridge Hydrodynamics (page images at HathiTrust)
• Langley Research Center: Stability analysis for laminar flow control, Part I (National Aeronautics and Space Administration ;, 1977), also by David J. Benney, Steven A. Orszag, inc Cambridge Hydrodynamics, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Stability analysis of plates and shells : a collection of papers in honor of Dr. Manuel Stein (National Aeronautics and Space Administration, Langley Research Center, 1998), also by Manuel Stein, Michael P. Nemeth, Norman F. Knight, and Structural Dynamics AIAA/ASME/ASCE/AHS/ASC Structures (page images at HathiTrust)
• Langley Research Center: Stability and control characteristics at a Mach number of 1.41 of a variable-sweep airplane configuration capable of low-level supersonic attack-outer wing swept 75 degree and 108 degree (National Aeronautics and Space Administration, 1960), also by Ross B. Robinson and Paul W. Howard (page images at HathiTrust)
• Langley Research Center: Stability and control characteristics at a mach number of 1.89 of a lightweight glider reentry configuration (National Aeronautics and Space Administration, 1960), also by Ross B. Robinson and M. Leroy Spearman (page images at HathiTrust)
• Langley Research Center: Stability and control characteristics at a Mach number of 1.97 of an airplane configuration having two types of variable- sweep wings (National Aeronautics and Space Administration, 1960), also by Gerald V. Foster, Odell A. Morris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Stability and control characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with outboard wing panels swept back 75° (National Aeronautics and Space Administration, 1959), also by M. Leroy Spearman, Gerald V. Foster, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Stability and control characteristics at low subsonic speeds of an airplane configuration having two types of variable-sweep wings (National Aeronautics and Space Administration, 1960), also by Bernard Spencer (page images at HathiTrust)
• Langley Research Center: Stability and control characteristics at Mach numbers from 0.20 to 4.63 of a cruciform air-to-air missile with triangular canard controls and a trapezoidal wing (National Aeronautics and Space Administration ;, 1974), also by Ernald B. Graves and Roger H. Fournier (page images at HathiTrust)
• Langley Research Center: Stability and control characteristics at mach numbers of 2.50, 3.00, and 3.71 of a variable- wing-sweep configuration with outboard wing panels swept back 75 degree (National Aeronautics and Space Administration, 1960), also by Gerald V. Foster and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Stability and control characteristics of a monoplanar elliptic missile model at Mach numbers from 1.60 to 2.86 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Wallace C. Sawyer, Giuliana Sangiorgio, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Milton Lamb and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45? (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by William P. Henderson, Laurence D. Leavitt, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Stability and control characteristics of an air-breathing missile configuration having a forward located inlet (National Aeronautics and Space Administration ;, 1976), also by Wallace C. Sawyer and Clyde Hayes (page images at HathiTrust)
• Langley Research Center: Stability boundaries for systems with frequency-model feedback and complementary filter (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1980), also by L. Keith Barker and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Stability characteristics for a full-span model at Mach 0.30 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Robert R. Meyer, United States Air Force, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Stability of multirate sampled-data systems (National Aeronautics and Space Administration ;, 1975), also by David P. Stanford, Alper K. Caglayan, and College of William and Mary (page images at HathiTrust)
• Langley Research Center: Stability of separating subsonic boundary layers (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Jamal A. Masad and Ali Hasan Nayfeh (page images at HathiTrust)
• Langley Research Center: Stagnation point heat transfer during hypervelocity atmospheric entry (National Aeronautics and Space Administration ;, 1970), also by W. S. Rigdon, M. Thomas, R. B. Dirling, and McDonnell Douglas Astronautics Company. Western Division (page images at HathiTrust)
• Langley Research Center: Stagnation-point shielding by melting and vaporization (U.S. G.P.O., 1959), also by Leonard Roberts and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Standard experiments in engineering materials science and technology (National Aeronautics and Space Administration Langley Research Center, 1995), also by Md.) National Educators' Workshop: Update 94 (1994 : Gaithersburg, A. C. Fraker, James A. Jacobs, James E. Gardner, United States. Department of Energy, Norfolk State University (Va.), United States National Aeronautics and Space Administration, and National Institute of Standards and Technology (U.S.) (page images at HathiTrust)
• Langley Research Center: Standardization, certification, maintenance, and dissemination of large scale engineering software systems : a panel discussion held as a part of the Second National Symposium on Computerized Structural Analysis and Design (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1977), also by Khalil Khozeimeh, Harvey G. McComb, Theodore G. Toridis, National Science Foundation (U.S.), and National Symposium on Computerized Structural Analysis and Design (2nd : 1976 : George Washington University) (page images at HathiTrust)
• Langley Research Center: Star adaptation for two-algorithms used on serial computers (National Aeronautics and Space Administration ;, 1974), also by Lona M. Howser and Jules J. Lambiotte (page images at HathiTrust)
• Langley Research Center: Static aerodynamic characeristics of a winged single-stage-to-orbit vehicle at Mach numbers from 0.3 to 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Delma C. Freeman, Roger H. Fournier, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Static aerodynamic characteristics of a 1/9-scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65 (National Aeronautics and Space Administration, 1962), also by Roger H. Fournier (page images at HathiTrust)
• Langley Research Center: Static aerodynamic characteristics of a model of a typical subsonic jet-transport airplane at Mach numbers from 0.40 to 1.20 (National Aeronautics and Space Administration ;, 1967), also by Eugene N. Brooks, James A. Blackwell, and John P. Decker (page images at HathiTrust)
• Langley Research Center: Static aerodynamic characteristics of three rocket-vehicle configurations at Mach numbers from 1.80 to 4.63 including some effects of fin size, fin cant, and auxiliary rocket motors (National Aeronautics and Space Administration, 1963), also by Dennis E. Fuller and Gerald V. Foster (page images at HathiTrust)
• Langley Research Center: Static and dynamic longitudinal stability derivatives of a powered 0.18 scale model of a fan-in-wing VTOL aircraft (National Aeronautics and Space Administration, 1968), also by Joseph R. Chambers, Sue B. Grafton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Static and wind-on tests of an upper-surface-blown jet-flap nozzle arrangement for use on the Quiet Clean Shore-haul Experimental Engine (QCSEE) (National Aeronautics and Space Administration ;, 1977), also by Arthur E. Phelps and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Static and yawed-rolling mechanical properties of two type VII aircraft tires (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John A. Tanner, John L. McCarty, Sandy M. Stubbs, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Static footprint local forces, areas, and aspect ratios for three type VII aircraft tires (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by William E. Howell, William A. Vogler, and Sharon E. Tanner (page images at HathiTrust)
• Langley Research Center: Static force tests of a model of a twin-jet fighter airplane for angles of attack from -10⁰ to 110⁰ and sideslip angles from -40⁰ to 40⁰ (National Aeronautics and Space Administration, 1971), also by Ernie L. Anglin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Laurence D. Leavitt, Richard J. Re, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Linda S. Bangert and Laurence D. Leavitt (page images at HathiTrust)
• Langley Research Center: Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Laurence D. Leavitt and James R. Burley (page images at HathiTrust)
• Langley Research Center: Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Richard J. Re and Laurence D. Leavitt (page images at HathiTrust)
• Langley Research Center: Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Laurence D. Leavitt (page images at HathiTrust)
• Langley Research Center: Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by George T. Carson and Francis J. Capone (page images at HathiTrust)
• Langley Research Center: Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Richard J. Re, Bobby L. Berrier, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Richard J. Re and George T. Carson (page images at HathiTrust)
• Langley Research Center: Static investigation of a two-dimensional convergent-divergent exhaust nozzle with multiaxis thrust-vectoring capability (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by John G. Taylor (page images at HathiTrust)
• Langley Research Center: Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by James R. Burley, John R. Carlson, and Linda S. Bangert (page images at HathiTrust)
• Langley Research Center: Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Mary L. Mason and Bobby L. Berrier (page images at HathiTrust)
• Langley Research Center: A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Mary L. Mason, Scott C. Asbury, and Francis J. Capone (page images at HathiTrust)
• Langley Research Center: Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Mary L. Mason and James R. Burley (page images at HathiTrust)
• Langley Research Center: Static lateral characteristics at high subsonic speeds of a complete airplane model with a highly tapered wing having the 0.80 chord line unswept and with several tail configuration. (National Aeronautics and Space Administration, 1961), also by Kenneth W. Goodson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Static longitudinal aerodynamic characteristics and surface pressure distributions for a 1/15-scale model of a modified four-stage Scout vehicle (National Aeronautics and Space Administration, 1963), also by Thomas C. Kelly (page images at HathiTrust)
• Langley Research Center: Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry (National Aeronautics and Space Administration, 1962), also by Lawrence E. Putnam and Cuyler W. Brooks (page images at HathiTrust)
• Langley Research Center: Static longitudinal aerodynamic characteristics at transonic speeds and angles of attack up to 99 degree of a reentry glider having folding wing-tip panels (National Aeronautics and Space Administration, 1961), also by Walter B. Olstad (page images at HathiTrust)
• Langley Research Center: Static longitudinal aerodynamic characteristics of close-coupled wing-canard configurations at Mach numbers from 1.60 to 2.86. (National Aeronautics and Space Administration :, 1971), also by Samuel M. Dollyhigh and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels (National Aeronautics and Space Administration, 1961), also by M. Leroy Spearman and Gerald V. Foster (page images at HathiTrust)
• Langley Research Center: Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a V/STOL airplane configuration with a variable-sweep wing and with a skewed wing design (National Aeronautics and Space Administration, 1961), also by Odell A. Morris and Gerald V. Foster (page images at HathiTrust)
• Langley Research Center: Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration (National Aeronautics and Space Administration, 1960), also by Gerald V. Foster, Odell A. Morris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Static longitudinal and lateral stability and control characteristics of a right triangular pyramidal lifting reentry configuration at Mach numbers from 2.36 to 4.65 (National Aeronautics and Space Administration, 1963), also by Nickolai Charczenko and C. Donald Babb (page images at HathiTrust)
• Langley Research Center: Static longitudinal characteristics at high subsonic speeds of a complete airplane model with a highly tapered wing having the 0.80 chord line unswept and with several tail configurations (National Aeronautics and Space Administration, 1961), also by Kenneth W. Goodson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Static longitudinal, directional, and lateral stability and control data at a mach number of 6.83 of the final configuration of the X-15 research airplane (National Aeronautics and Space Administration, 1960), also by Jim A. Penland and Jr. Fetterman (page images at HathiTrust)
• Langley Research Center: Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces (National Aeronautics and Space Administration, 1961), also by Ross B. Robinson and Gerald V. Foster (page images at HathiTrust)
• Langley Research Center: Static longitudinal stability of a rocket vehicle having a rear-facing step ahead of the stabilizing fins (National Aeronautics and Space Administration, 1961), also by Robert J. Keynton and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Static mechanical properties of 30 x 11.5 - 14.5, type VIII aircraft tires of bias-ply and radial-belted design (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Pamela A. Davis and Mercedes C. Lopez (page images at HathiTrust)
• Langley Research Center: Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by David J. Wing and Scott C. Asbury (page images at HathiTrust)
• Langley Research Center: Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Bobby L. Berrier (page images at HathiTrust)
• Langley Research Center: Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Mary L. Mason and Bobby L. Berrier (page images at HathiTrust)
• Langley Research Center: Static stability and control characteristics of two large-dihedral right triangular pyramid lifting reentry configurations at a mach number of 3.05 (National Aeronautics and Space Administration, 1960), also by Charles F. Whitcomb and Willard E. Foss (page images at HathiTrust)
• Langley Research Center: Static stability and separation characteristics of a two-stage rocket configuration at Mach numbers from 1.57 to 4.50 (National Aeronautics and Space Administration, 1960), also by Kenneth L. Turner, Laurence W. Enderson, and David S. Shaw (page images at HathiTrust)
• Langley Research Center: Static stability characteristics of models of the Blue Scout and the Blue Scout, Jr., research vehicles at Mach numbers from 2.29 to 3.75 (National Aeronautics and Space Administration, 1963), also by Lloyd S. Jernell (page images at HathiTrust)
• Langley Research Center: The static stability characteristics of several preliminary models of the X-15 research airplane at Mach numbers of 2.98 and 4.01 (National Aeronautics and Space Administration, 1959), also by Robert W. Dunning and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Static structural tests of a 1.5-meter-diameter fabric attached inflatable decelerator (National Aeronautics and Space Administration ;, 1972), also by Conrad M. Willis and Martin M. Mikulas (page images at HathiTrust)
• Langley Research Center: Static, subsonic, and supersonic oxidation of JT graphite composites (National Aeronautics and Space Administration ;, 1967), also by John D. Buckley (page images at HathiTrust)
• Langley Research Center: Static tests of a simulated upper surface blown jet-flap configuration utilizing a full-size turbofan engine (National Aeronautics and Space Administration ;, 1975), also by James P. Shivers and Charles C. Smith (page images at HathiTrust)
• Langley Research Center: Static tests of excess ground attenuation at Wallops Flight Center (National Aeronautical and Space Administration, Scientific and Technical Information Branch ;, 1981), also by L. C. Sutherland, Ron Brown, Wallops Flight Center, Wyle Research (Firm), and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Static thrust augmentation of a rocket-ejector system with a heated supersonic primary jet (National Aeronautics and Space Administration, 1962), also by Albert J. Simonson, James W. Schmeer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Robert J. Foley and Odis C. Pendergraft (page images at HathiTrust)
• Langley Research Center: Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Long P. Yip (page images at HathiTrust)
• Langley Research Center: Statistical analysis of meteoroid penetration data including effects of cutoff (National Aeronautics and Space Administration ;, 1970), also by J. M. Alvarez (page images at HathiTrust)
• Langley Research Center: Statistical comparisons of aircraft flyover noise adjustment procedures for different weather conditions (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Arnold W. Mueller, David A. Hilton, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Statistical evaluation of aircraft collision-hazard warning system techniques in the terminal area : phase II. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1969), also by Research Triangle Institute and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A Statistical model for synthetic wind profiles for aerospace vehicle design and launching criteria (National Aeronautics and Space Administration, 1963), also by Robert M. Henry and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: A statistical study of ability of simulated pilots to control the approach and descent of the lunar module to the lunar surface (National Aeronautics and Space Administration, 1971), also by Jacob H. Lichtenstein and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Statistical wind distribution data for use at NASA Wallops Station (National Aeronautics and Space Administration, 1962), also by William L. Weaver, John F. Spurling, Andrew G. Swanson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Statistics of solar cosmic rays as inferred from correlation with intense geomagnetic storms (National Aeronautics and Space Administration, 1962), also by David Adamson and Robert E. Davidson (page images at HathiTrust)
• Langley Research Center: Statistics of some atmospheric turbulence records relevant to aircraft response calculations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by William D. Mark, Raymond W. Fischer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Status of linear boundary-layer stability theory and the en method, with emphasis on swept-wing applications (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Jerry N. Hefner, Dennis M. Bushnell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Steady and unsteady aerodynamic forces from the SOUSSA surface-panel method for a fighter wing with tip missile and comparison with experiment and PANAIR (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Herbert J. Cunningham (page images at HathiTrust)
• Langley Research Center: Steady-state and transitional aerodynamic characteristics of a wing in simulated heavy rain (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Bryan A. Campbell and Gaudy M. Bezos (page images at HathiTrust)
• Langley Research Center: Steady subsonic flow around finite-thickness wings (National Aeronautics and Space Administration ;, 1975), also by Ching-Chiang Kuo, L. Morino, and Boston University. Dept. of Aerospace Engineering (page images at HathiTrust)
• Langley Research Center: Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Russell V. Parrish, Steven P. Williams, United States. Army Aviation Systems Command, and United States. Army Aviation Research and Development Command (page images at HathiTrust)
• Langley Research Center: Stiffness and strength tailoring in uniform space-filling truss structures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Mark S. Lake (page images at HathiTrust)
• Langley Research Center: Stochastic analysis of spectral broadening by a free turbulent shear layer (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Jay C. Hardin, John S. Preisser, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: STOL ride control feasibility study : technical report (National Aeronautics and Space Administration ;, 1973), also by C. K. Gordon, R. O. Dodson, and Boeing Company. Wichita Division (page images at HathiTrust)
• Langley Research Center: Strain-gage bridge calibration and flight loads measurements on a low-aspect-ratio thin wing (National Aeronautics and Space Administration ;, 1975), also by Ellwood L. Peele and Clinton V. Eckstrom (page images at HathiTrust)
• Langley Research Center: Strain-rate sensitivity of three titanium-alloy sheet materials after prolonged exposure at 550 ̊F (561 ̊K) (National Aeronautics and Space Administration ;, 1969), also by Robert M. Baucom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Stratospheric emissions effects database development (National Aeronautics and Space Administration, Langley Research Center ;, 1994), also by Steven L. Baughcum (page images at HathiTrust)
• Langley Research Center: Streamline curvature design procedure for subsonic and transonic ducts (National Aeronautics and Space Administration ;, 1973), also by Raymond L. Barger (page images at HathiTrust)
• Langley Research Center: A streamline curvature method for design of supercritical and subcritical airfoils (National Aeronautics and Space Administration ;, 1974), also by Raymond L. Barger and Cuyler W. Brooks (page images at HathiTrust)
• Langley Research Center: Streamlined design and self reliant hardware for active control of precision space structures (National Aeronautics and Space Administration, Langley Research Center ;, 1994), also by David C. Hyland, Douglas J. Phillips, and James A. King (page images at HathiTrust)
• Langley Research Center: Strength evaluation of socket joints (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Larry C. Rash (page images at HathiTrust)
• Langley Research Center: Strength of graphite/epoxy bolted wing-skin splice specimens subjected to outdoor exposure under constant load and yearly fatigue loading (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Gregory R. Wichorek and John H. Crews (page images at HathiTrust)
• Langley Research Center: Stress analysis and buckling of J-stiffened graphite-epoxy panel. (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Randall C. Davis and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Stress concentration around broken filaments in a filament-stiffened sheet (National Aeronautics and Space Administration, 1969), also by W. B. Fichter and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Stress-concentration factors for finite orthotropic laminates with a circular hole and uniaxial loading (National Aeronautics and Space Administration, Scientifice and Technical Information Office, 1979), also by C. S. Hong, John H. Crews, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Stress-concentration factors for finite orthotropic laminates with a pin-loaded hole (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1981), also by John H. Crews, I. S. Raju, C. S. Hong, Joint Institute for Advancement of Flight Sciences, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Stress concentrations for straight-shank and countersunk holes in plates subjected to tension, bending, and pin loading (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by K. N. Shivakumar and J. C. Newman (page images at HathiTrust)
• Langley Research Center: Stress-corrosion cracking of Ti-6Al-4V titanium alloy in nitrogen tetroxide (National Aeronautics and Space Administration ;, 1968), also by W. Barry Lisagor, Thomas T. Bales, and Charles R. Manning (page images at HathiTrust)
• Langley Research Center: Structural analysis of three space crane articulated-truss joint concepts (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by K. Chauncey Wu and Thomas R. Sutter (page images at HathiTrust)
• Langley Research Center: Structural characterization of a first-generation articulated-truss joint for space crane application (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Thomas R. Sutter (page images at HathiTrust)
• Langley Research Center: Structural concepts for hydrogen-fueled hypersonic airplanes (National Aeronautics and Space Administration, 1966), also by L. Robert Jackson, Gregory R. Wichorek, John G. Davis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Structural concepts for large solar concentrators (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by John M. Hedgepeth, Richard K. Miller, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Astro Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Structural dynamic experiences of the X-15 airplane (National Aeronautics and Space Administration, 1962), also by Gareth H. Jordan, Lawrence D. Guy, Norman J. McLeod, United States National Aeronautics and Space Administration, Flight Research Center (U.S.), and Calif.) Conference on the Progress of the X-15 Project (1961 : Edwards Air Force Base (page images at HathiTrust)
• Langley Research Center: Structural dynamics and control of large space structures, 1982 : proceedings of a workshop held at NASA Langley Research Center, Hampton, Virginia, January 21-22, 1982 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by M. Larry Brumfield and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Structural Dynamics Division research and technology accomplishments for FY 1988 and plans for FY 1989. (Langley Research Center, 1989), also by James E. Gardner and Langley Research Center. Structures and Dynamics Division (page images at HathiTrust)
• Langley Research Center: Structural integrity evaluation of the Lear Fan 2100 aircraft (Federal Aviation Administration, Office of Aviation Research ;, 1996), also by H. P. Kan, T. A. Dyer, Northrop Corporation. Military Aircraft Division, and United States. Office of Aviation Research (page images at HathiTrust)
• Langley Research Center: Structural modeling of aircraft tires (National Aeronautics and Space Administration ;, 1973), also by Samuel K. Clark and University of Michigan (page images at HathiTrust)
• Langley Research Center: Structural optimization of sandwich and ring-stiffened 120 degree conical shells subjected to external pressure (National Aeronautics and Space Administration ;, 1969), also by Gerald A. Cohen and Philco-Ford Corporation (page images at HathiTrust)
• Langley Research Center: Structural performance of two aerobrake hexagonal heat shield panel concepts (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by John T. Dorsey and James W. Dyess (page images at HathiTrust)
• Langley Research Center: Structural properties of bismuth-bearing semiconductor alloys (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986), also by Martha A. Berding, A.-B. Chen, and A. Sher (page images at HathiTrust)
• Langley Research Center: Structure-borne noise estimates for the PTA aircraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by James F. Unruh and Southwest Research Institute (page images at HathiTrust)
• Langley Research Center: Structures for reentry heating (National Aeronautics and Space Administration, 1961), also by Roger A. Anderson and Robert T. Swann (page images at HathiTrust; US access only)
• Langley Research Center: Studies of condensation effects on airfoil testing in the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Robert M. Hall (page images at HathiTrust)
• Langley Research Center: Studies of friction and wear characteristics of various wires for wire-brush skids (National Aeronautics and Space Administration ;, 1977), also by Robert C. Dreher and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Studies of optimum body shapes at hypersonic speeds (National Aeronautics and Space Administration, 1967), also by Louis S. Stivers, Bernard Spender, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suction (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by A. V. Murthy and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Studies relating to temperature control of a large space telescope (National Aeronautics and Space Administration ;, 1973), also by S. Katzoff (page images at HathiTrust)
• Langley Research Center: Study and development of acoustic treatment for jet engine tailpipes (National Aeronautics and Space Administration, 1971), also by M. D. Nelsen, Boeing Company. AVCO Corporation. Systems Division, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A study for development of aerothermodynamic test model materials and fabrication technique (National Aeronautics and Space Administration ;, 1972), also by W. G. Dean, L. E. Connor, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Langley Research Center: Study of a fail-safe abort system for an actively cooled hypersonic aircraft : volume I--technical summary (U.S. National Aeronautics and Space Administration ;, 1976), also by C. J. Pirrello, R. L. Herring, United States National Aeronautics and Space Administration, and McDonnell Douglas Corporation (page images at HathiTrust)
• Langley Research Center: A study of abort from a manned lunar landing and return to rendezvous in a 50-mile orbit (National Aeronautics and Space Administration, 1962), also by Jack A. White and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Study of advanced composite structural design concepts for an arrow wing supersonic cruise configuration (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by M. J. Turner, D. L. Grande, Boeing Commercial Airplane Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Study of aircraft-centered navigation, guidance, and traffic situation system concept for terminal-area operation (National Aeronautics and Space Administration ;, 1972), also by Willard W. Anderson, Carolyn Grantham, and Ralph W. Will (page images at HathiTrust)
• Langley Research Center: A study of aluminum-lithium alloy solidification using acoustic emission techniques (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Daniel P. Henkel and Lehigh University (page images at HathiTrust)
• Langley Research Center: Study of an automatic system for control of the terminal phase of satellite rendezvous (U.S. G.P.O., 1962), also by Edgar C. Lineberry, Edwin C. Foudriat, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Study of an automatic system for control of the terminal phase of satellite rendezvous (U.S. G.P.O., 1962), also by Edgar C. Lineberry, Edwin C. Foudriat, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A study of aseptic maintenance by pressurization (National Aeronautics and Space Administration ;, 1971), also by D. J. Cheater and General Electric Company. Re-entry and Environmental Systems Division (page images at HathiTrust)
• Langley Research Center: Study of astronaut capabilities to perform extravehicular maintenance and assembly functions in weightless conditions (National Aeronautics and Space Administration, 1967), also by E. C. Wortz, AiResearch Manufacturing Company of Los Angeles (Calif.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A study of beryllium and beryllium-lithium complexes in single-crystal silicon (National Aeronautics and Space Administration ;, 1972), also by Roger K. Crouch, T. E. Gilmer, and James B. Robertson (page images at HathiTrust)
• Langley Research Center: A study of boundary layer transition on outgassing cones in hypersonic flow (National Aeronautics and Space Administration, 1971), also by C. J. Stalmach, United States National Aeronautics and Space Administration, and Vought Aeronautics Company (page images at HathiTrust)
• Langley Research Center: A study of canard-wing interference using experimental pressure data at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Blair B. Gloss, Karen E. Washburn, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Study of coaxial Hall current accelerators at moderate pressures (National Aeronautics and Space Administration ;, 1966), also by H. A. Hassan, William Grossmann, Robert V. Hess, and North Carolina State University (page images at HathiTrust)
• Langley Research Center: A study of crack closure in fatigue (National Aeronautics and Space Administration ;, 1973), also by T. T. Shih, Robert Peh-ying Wei, and Lehigh University (page images at HathiTrust)
• Langley Research Center: Study of critical defects in ablative heat shield systems for the space shuttle (National Aeronautics and Space Administration ;, 1972), also by R. L. Thompson, W. E. Driver, Ward D. Rummel, and Martin Marietta Denver Aerospace (page images at HathiTrust)
• Langley Research Center: A study of dynamic tire properties over a range of tire constructions (National Aeronautics and Space Administration ;, 1973), also by G. H. Nybakken, Samuel K. Clark, and University of Michigan (page images at HathiTrust)
• Langley Research Center: A study of equilibrium real-gas effects in hypersonic air nozzles, including charts of thermodynamic properties for equilibrium air (National Aeronautics and Space Administration, 1960), also by Wayne D. Erickson and Helen S. Creekmore (page images at HathiTrust)
• Langley Research Center: A study of factors affecting the accuracy of the position fix for lunar trajectories (National Aeronautics and Space Administration :, 1964), also by Margery E. Hannah and Alton P. Mayo (page images at HathiTrust)
• Langley Research Center: A Study of flight control requirements for advanced, winged, earth-to-orbit vehicles with far-aft center-of-gravity locations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Study of high-speed civil transports (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Douglas Aircraft Company. New Commercial Programs (page images at HathiTrust)
• Langley Research Center: Study of high-speed civil transports : summary (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Douglas Aircraft Company. New Commercial Programs (page images at HathiTrust)
• Langley Research Center: Study of lee-side flows over conically cambered delta wings at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Richard M. Wood and Carolyn B. Watson (page images at HathiTrust)
• Langley Research Center: Study of liquid-phase epitaxy methods for growth of InGaAsP/InP CW lasers (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by I. Ladany and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Study of low pressure application of new orbitron and ion gauge designs (National Aeronautics and Space Administration] ;, 1969), also by Charles M. Gosselin, Mo.) Midwest Research Institute (Kansas City, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Study of man pulling a cart on the moon (National Aeronautics and Space Administration, 1971), also by A. Camacho, A. Walther, W. Robertson, and AiResearch Manufacturing Company of Los Angeles (Calif.) (page images at HathiTrust; US access only)
• Langley Research Center: A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number (National Aeronautics and Space Administration ;, 1973), also by Robert J. Mack (page images at HathiTrust)
• Langley Research Center: A study of NACA and NASA published information of pertinence in the design of light aircraft. Volume II, Aerodynamics and aerodynamic loads (National Aeronautics and Space Administration ;, 1970), also by James C. Williams, John N. Perkins, Delbert C. Summey, and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• Langley Research Center: A study of NACA and NASA published information of pertinence in the design of light aircraft. Volume III, Propulsion subsystems, performance, stability and control, propellers, and flight safety (National Aeronautics and Space Administration ;, 1970), also by Clifford J. Moore, Dennis M. Phillips, and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• Langley Research Center: Study of new methods to measure low pressure. (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), also by Richard Hecht and National Research Corporation (U.S.) (page images at HathiTrust)
• Langley Research Center: Study of noise sources in a subsonic fan using measured blade pressures and acoustic theory (National Aeronautics and Space Administration ;, 1975), also by Donald B. Hanson and United Technologies Corporation. Hamilton Standard Division (page images at HathiTrust)
• Langley Research Center: A study of oxidation kinetics of nickel metal in flowing air and oxygen-nitrogen mixtures (National Aeronautics and Space Administration :, 1964), also by Donald J. Progar and Beverley W. Lewis (page images at HathiTrust)
• Langley Research Center: A study of panel loads and centers of pressure of three different cruciform aft-tail control surfaces of a wingless missile from March 1.60 to 3.70 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Milton Lamb, Charles D. Trescot, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A study of personnel propulsion devices for use in the vicinty of the moon (National Aeronautics and Space Administration;, 1966), also by N. Economou and Bell Aerospace Corporation. Bell Aerosystems Company (page images at HathiTrust)
• Langley Research Center: Study of photon correlation techniques for processing of laser velocimeter signals (National Aeronautics and Space Administration ;, 1977), also by William T. Mayo, inc Science Applications, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Study of physiological and behavioral response to transitions between rotating and nonrotating environments (National Aeronautics and Space Administration ;, 1972), also by James F. Brady and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Langley Research Center: A study of radiometric emission from a rough sea surface (National Aeronautics and Space Administration ;, 1972), also by A. Stogryn and Aerojet-General Corporation. Microwave Division (page images at HathiTrust)
• Langley Research Center: A study of residual interference effects in adaptive wall testing of a 7-inch chord CAST-10-2/DOA 2 airfoil model (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by A. V. Murthy and Inc ViGYAN (page images at HathiTrust)
• Langley Research Center: A Study of scattering, production, and stimulated emission of sound by vortex flows (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by John E. Yates and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A study of several oxidation-resistant coatings on Cb-10Ti-5Zr alloy sheet at 2000 ̊F, 2400 ̊F, and 2700 ̊F (1365 ̊K, 1590 ̊K, and 1755 ̊K) (National Aeronautics and Space Administration ;, 1966), also by W. Barry Lisagor and Bland A. Stein (page images at HathiTrust)
• Langley Research Center: A study of some transition matrix assumptions in circumlunar navigation theory (National Aeronautics and Space Administration, 1963), also by Ruben L. Jones and Alton P. Mayo (page images at HathiTrust)
• Langley Research Center: Study of stability of large maneuvers of airplanes (National Aeronautics and Space Administration, 1974), also by Emile K. Haddad and Lockheed-Georgia Company (page images at HathiTrust)
• Langley Research Center: Study of supersonic wings employing the attainable leading-edge thrust concept (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by W. D. Middleton, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: A study of the accuracy of estimating the orbital elements of a lunar satellite by using range and range-rate measurements (National Aeronautics and Space Administration ;, 1966), also by Harold R. Compton (page images at HathiTrust)
• Langley Research Center: A study of the acoustic fatigue characteristics of some flat and curved aluminum panels exposed to random and discrete noise (National Aeronautics and Space Administration, 1959), also by R. W. Hess, William H. Mayes, and Robert W. Herr (page images at HathiTrust)
• Langley Research Center: Study of the application of a photoionization mass spectrometer to analysis of contaminant gases (National Aeronautics and Space Administration ;, 1970), also by Peter Warneck, C. Matthews, John N. Driscoll, and GCA Corporation (page images at HathiTrust)
• Langley Research Center: A study of the application of heat or force fields to the sonic-boom-minimization problem (National Aeronautics and Space Administration, 1969), also by David S. Miller, Harry W. Carlson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A Study of the application of singular perturbation theory (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Raman K. Mehra and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A study of the cornering forces generated by aircraft tires on a tilted, free-swiveling nose gear (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Robert H. Daugherty and Sandy M. Stubbs (page images at HathiTrust)
• Langley Research Center: A study of the dynamics of airplane braking systems as affected by tire elasticity and brake response (National Aeronautics and Space Administration ;, 1965), also by Sidney A. Batterson (page images at HathiTrust)
• Langley Research Center: A study of the effect of errors in measurement of velocity and flight-path angle on the guidance of a space vehicle approaching the earth (National Aeronautics and Space Administration, 1961), also by Jack A. White and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A Study of the effect of flight density and background noise on V/STOL acceptability (National Aeronautics and Space Administration ;, 1974), also by Harry Sternfeld and Boeing Vertol Company (page images at HathiTrust)
• Langley Research Center: A study of the effect of measurement errors upon a range controller for an entry vehicle (National Aeronautics and Space Administration ;, 1968), also by Jack A. White (page images at HathiTrust)
• Langley Research Center: A study of the feasibility of directly applying gas generator systems to space shuttle mechanical functions (National Aeronautics and Space Administration ;, 1974), also by E. Raymond Lake and McDonnell Aircraft Company (page images at HathiTrust)
• Langley Research Center: A study of the feasibility of statistical analysis of airport performance simulation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Raymond H. Myers and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A study of the guidance of a space vehicle returning to a braking ellipse about the earth (National Aeronautics and Space Administration, 1960), also by Jack A. White and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A study of the Markov game approach to tactical maneuvering problems (National Aeronautics and Space Administration ;, 1972), also by S. Baron, Saul Serbin, David L. Kleinman, and Beranek Bolt (page images at HathiTrust)
• Langley Research Center: Study of the modifications needed for effective operation of NASTRAN on IBM virtual storage computers (National Aeronautics and Space Administration ;, 1975), also by C. W. McCormick, K. H. Redner, and MacNeal-Schwendler Corporation (page images at HathiTrust)
• Langley Research Center: Study of the optimum values of several parameters affecting longitudinal handling qualities of VTOL aircraft (National Aeronautics and Space Administration, 1968), also by James R. Kelly, John F. Garren, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A study of the oxidation of materials in an arc-image furnace (National Aeronautics and Space Administration, 1961), also by R. Gale Wilson, A. J. McEvily, and Roger W. Peters (page images at HathiTrust)
• Langley Research Center: A Study of the positions and velocities of a space station and a ferry vehicle during rendezvous and return (U.S. G.P.O., 1961), also by John M. Eggleston, Harold D. Beck, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A study of the possible characteristics of a low-altitude electron layer in the Martian atmosphere (National Aeronautics and Space Administration ;, 1974), also by H. Andrew Wallio (page images at HathiTrust)
• Langley Research Center: Study of the reaction of atomic oxygen with aerosols (National Aeronautics and Space Administration, 1975), also by Francis I. Akers, James P. Wightman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A study of the role of pyrotechnic systems on the space shuttle program (National Aeronautics and Space Administration ;, 1973), also by E. Raymond Lake, V. W. Drexelius, S. J. Thompson, and McDonnell Douglas Corporation (page images at HathiTrust)
• Langley Research Center: A study of the sonic-boom characteristics of a blunt body at a Mach number of 4.14 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Harry W. Carlson, Robert J. Mack, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by George C. Ashby and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Study of the use of terminal control techniques for guidance during direct and skip entries for a capsule-type vehicle at parabolic velocity (National Aeronautics and Space Administration :, 1964), also by John W. Young (page images at HathiTrust)
• Langley Research Center: A study of the viscous dissipation and surface loading on a vibrating surface (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John E. Yates and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Study on advanced information processing system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Kang G. Shin, Jyh-Charn Liu, and University of Michigan (page images at HathiTrust)
• Langley Research Center: A study to determine the flight characteristics and handling qualities of variable geometry spacecraft. Volume III, Low L/D concept with fold-down wings (National Aeronautics and Space Administration ;, 1972), also by George R. Friedman, B. J. Kuchta, and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Langley Research Center: Study to determine the IFR operational profile and problems of the general aviation single pilot (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by G. S. Weislogel, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Ohio State University (page images at HathiTrust)
• Langley Research Center: A study to investigate the chemical stability of gallium phosphate oxide/gallium arsenide phosphide (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Gordon J. Kuhlmann and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Subjective assessment of simulated helicopter blade-slap noise (National Aeronautics and Space Administration ;, 1976), also by Ben William Lawton and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The subjective evaluation of noise from light aircraft. (National Aeronautics and Space Administration ;, 1976), also by Kevin P. Shepherd, University of Utah. Dept. of Mechanical and Industrial Engineering, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A subjective evaluation of synthesized STOL airplane noises (National Aeronautics and Space Administration ;, 1973), also by Clemans A. Powell (page images at HathiTrust)
• Langley Research Center: Subjective field study of response to impulsive helicopter noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Clemans A. Powell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Subjective response to combined noise and vibration during flight of a large twin-jet airplane (U.S. National Aeronautics and Space Administration ;, 1976), also by Sherman A. Clevenson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Subjective response to synthesized flight noise signatures of several types of V/STOL aircraft (National Aeronautics and Space Administration ;, 1968), also by Ernest G. Hinterkeuser, Harry Sternfeld, and Boeing Company (page images at HathiTrust)
• Langley Research Center: Subsolar-meridian mean-annual distributions for Martian troposphere below 50 kilometers (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information Springfield, Va., 1968), also by Ferdinand Charles Bates and St. Louis University (page images at HathiTrust)
• Langley Research Center: Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex (National Aeronautics and Space Administration :, 1965), also by Edward C. Polhamus, Alexander D. Hammond, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Subsonic aerodynamic characteristics of interacting lifting surfaces with separated flow around sharp edges predicted by a vortex-lattice method (National Aeronautics and Space Administration ;, 1975), also by John E. Lamar and Blair B. Gloss (page images at HathiTrust)
• Langley Research Center: Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage (National Aeronautics and Space Administration ;, 1974), also by Samuel M. Dollyhigh (page images at HathiTrust)
• Langley Research Center: Subsonic and supersonic static aerodynamic characteristics of a family of bulbous base cones measured with a magnetic suspension and balance system (National Aeronautics and Space Administration ;, 1972), also by Milan Vlajinac and Massachusetts Institute of Technology (page images at HathiTrust)
• Langley Research Center: Subsonic and transonic dynamic stability characteristics of a space shuttle orbiter (National Aeronautics and Space Administration ;, 1975), also by Richmond P. Boyden and Delma C. Freeman (page images at HathiTrust)
• Langley Research Center: Subsonic and transonic dynamic-stability characteristics of the space shuttle launch vehicle (U.S. National Aeronautics and Space Administration ;, 1976), also by Delma C. Freeman, Edwin E. Davenport, and Richmond P. Boyden (page images at HathiTrust)
• Langley Research Center: Subsonic annular wing theory with application to flow about nacelles (National Aeronautics and Space Administration ;, 1974), also by Michael J. Mann (page images at HathiTrust)
• Langley Research Center: Subsonic characteristics of a twin-jet swept-wing fighter model with maneuvering devices (National Aeronautics and Space Administration ;, 1973), also by Edward J. Ray and Eddie G. Hollingsworth (page images at HathiTrust)
• Langley Research Center: Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Richmond P. Boyden and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47⁰ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Michael J. Mann, Charles H. Fox, and Jarrett K. Huffman (page images at HathiTrust)
• Langley Research Center: Subsonic maneuver capability of a supersonic cruise fighter wing concept (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Gregory D. Riebe and Charles H. Fox (page images at HathiTrust)
• Langley Research Center: Subsonic panel method for designing wing surfaces from pressure distribution (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by D. R. Bristow, J. Dennis Hawk, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Subsonic panel method for the efficient analysis of multiple geometry perturbations (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982), also by D. R. Bristow, J. Dennis Hawk, and McDonnell Aircraft Company (page images at HathiTrust)
• Langley Research Center: Subsonic roll-damping characteristics of a series of wings (National Aeronautics and Space Administration ;, 1974), also by Richmond P. Boyden (page images at HathiTrust)
• Langley Research Center: Subsonic sting interference on the aerodynamic characteristics of a family of slanted-base ogive-cylinders (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Colin P. Britcher, W. Allen Kilgore, Charles W. Alcorn, and Old Dominion University. Dept. of Mechanical Engineering and Mechanics (page images at HathiTrust)
• Langley Research Center: Subsonic tests of an all-flush-pressure-orifice air data system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Terry J. Larson, Paul M. Siemers, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Hugh L. Dryden Flight Research Center (page images at HathiTrust)
• Langley Research Center: Subsonic wind-tunnel investigation of a twin-engine attack airplane model having nonmetric powered nacelles (National Aeronautics and Space Administration ;, 1974), also by Vernard E. Lockwood and Aniello Matarazzo (page images at HathiTrust)
• Langley Research Center: Subsonic wind-tunnel tests of a trailing-cone device for calibrating aircraft static-pressure systems (National Aeronautics and Space Administration ;, 1973), also by Frank L. Jordan and Virgil S. Ritchie (page images at HathiTrust)
• Langley Research Center: Substructure coupling for dynamic analysis and testing (National Aeronautics and Space Administration ;, 1977), also by Roy R. Craig, Ching-Jone Chang, University of Texas at Austin, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A summary and integration of research concerning single pilot IFR operational problems (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by G. Courtney Chapman, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Ohio State University (page images at HathiTrust)
• Langley Research Center: Summary of 1978 Southeastern Virginia Urban Plume Study : aircraft results for carbon monoxide, methane, nonmethane hydrocarbons, and ozone (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Gerald F. Hill, Wesley R. Cofer, Glen W. Sachse, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Summary of aircraft results for 1978 Southeastern Virginia Urban Plume Measurement Study of ozone, nitrogen oxides, and methane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Gerald L. Gregory and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Summary of available information on Reynolds analogy for zero-pressure-gradient, compressible, turbulent-boundary-layer flow (National Aeronautics and Space Administration ;, 1970), also by Aubrey M. Cary and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Summary of design considerations for airplane spin-recovery parachute systems (National Aeronautics and Space Administration ;, 1972), also by Sanger M. Burk (page images at HathiTrust)
• Langley Research Center: Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by John W. Paulson, James L. Thomas, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Summary of measurement results of ozone, methane, and nonmethane hydrocarbons for C-54 aircraft : 1979 southeastern Virginia urban plume study (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Wesley R. Cofer, Gerald L. Gregory, Gerald C. Purgold, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A summary of results on sonic-boom pressure-signature variations associated with atmospheric conditions (National Aeronautics and Space Administration, 1968), also by I. E. Garrick, Domenic J. Maglieri, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Summary of roll controls applicable to fin-stabilized vehicles (National Aeronautics and Space Administration :, 1964), also by Eugene D. Schult and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Summary of sonic boom rise times observed during FAA community response studies over a 6-month period in the Oklahoma City area (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Domenic J. Maglieri, Victor E. Sothcott, and Eagle Engineering (Firm) (page images at HathiTrust)
• Langley Research Center: Summary of southeastern Virginia urban plume measurement data for August 4 and 5, 1977 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by H. Scott Wagner, Gerald L. Gregory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Summary of spin technology as related to light general-aviation airplanes (National Aeronautics and Space Administration, 1971), also by James S. Bowman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A summary of the skylab crew : vehicle disturbances experiment T-013 (U.S. National Aeronautics and Space Administration ;, 1976), also by Bruce A. Conway and T. C. Hendricks (page images at HathiTrust)
• Langley Research Center: Summary of VGH and V-G data obtained from piston-engine transport airplanes from 1947 to 1958 (National Aeronautics and Space Administration, 1959), also by Walter G. Walker and Martin R. Copp (page images at HathiTrust)
• Langley Research Center: A summation and inhibition model of annoyance response to multiple community noise sources (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Clemans A. Powell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Supersonic aerodynamic characteristics of a 1/6-scale model of the final two stages of the Argo D-4 four-stage rocket vehicle (National Aeronautics and Space Administration ;, 1965), also by Clyde Hayes and William A. Corlett (page images at HathiTrust)
• Langley Research Center: Supersonic aerodynamic characteristics of a low-drag aircraft configuration having an arrow wing of aspect ratio 1.86 and a body of fineness ratio 20 (National Aeronautics and Space Administration :, 1960), also by Warren Gillespie Jr. (page images at HathiTrust)
• Langley Research Center: Supersonic aerodynamic characteristics of a proposed assured crew return capability (ACRC) lifting-body configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by George M. Ware (page images at HathiTrust)
• Langley Research Center: Supersonic aerodynamic characteristics of a Saturn IB launch vehicle model with third-stage modifications (National Aeronautics and Space Administration ;, 1966), also by Roger H. Fournier (page images at HathiTrust)
• Langley Research Center: Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Peter F. Covell (page images at HathiTrust)
• Langley Research Center: Supersonic aerodynamics of delta wings (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Richard M. Wood (page images at HathiTrust)
• Langley Research Center: A Supersonic area rule and an application to the design of a wing-body combination with high lift-drag ratios (U.S. G.P.O., 1960), also by Richard T. Whitcomb, John R. Sevier, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Supersonic cruise military aircraft research : an annotated bibliography (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Marie H. Tuttle, Dal V. Maddalon, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Supersonic dynamic stability characteristics of a space shuttle orbiter (National Aeronautics and Space Administration ;, 1976), also by Delma C. Freeman, Edwin E. Davenport, and Richmond P. Boyden (page images at HathiTrust)
• Langley Research Center: Supersonic dynamic-stability derivatives of the space shuttle launch vehicle (National Aeronautics and Space Administration ;, 1976), also by Richmond P. Boyden, Edwin E. Davenport, and Delma C. Freeman (page images at HathiTrust)
• Langley Research Center: Supersonic free-flight measurements of heat transfer and transition on a 10° cone having a low temperature ratio (National Aeronautical and Space Administration, 1961), also by Charles F. Merlet, Charles B. Rumsey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Supersonic investigation of nozzle hinge moments of a modified Saturn C-1 model with and without jet flow (National Aeronautics and Space Administration, 1963), also by Nickolai Charczenko and Jerry L. Lowery (page images at HathiTrust)
• Langley Research Center: Supersonic longitudinal stability characteristics of the two final stages of a four-stage launch vehicle (National Aeronautics and Space Administration :, 1964), also by Royce L. McKinney (page images at HathiTrust)
• Langley Research Center: Supersonic stability and control characteristics of a cruciform missile model with delta wings and aft tail fin controls (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by William A. Corlett and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A supersonic three-dimensional code for flow over blunt bodies : program documentation and test cases (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by D. S. Chaussee, Oden J. McMillan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A supersonic, three-dimensional code for flow over blunt bodies : user's manual (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by D. S. Chaussee, Oden J. McMillan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: The supersonic transport : a technical summary (National Aeronautics and Space Administration, 1960), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Supersonic transport operating practices during simulated operations in future air traffic control system environments (National Aeronautics and Space Administration ;, 1969), also by Milton D. McLaughlin, Richard H. Sawyer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Supersonic turbulent boundary-layer flows with mass injection through slots and/or porous walls (National Aeronautics and Space Administration ;, 1975), also by Alvin L. Murray and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Langley Research Center: Supersonic wings with significant leading-edge thrust at cruise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by A. Warner Robins, Robert J. Mack, Harry W. Carlson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Support interference of wind tunnel models : a selective annotated bibliography (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Marie H. Tuttle, Blair B. Gloss, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Surface effects on hydrogen permeation through Ti-14Al-21Nb alloy (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Sankara Narayan Sankaran, Ronald K. Clark, and R. A. Outlaw (page images at HathiTrust)
• Langley Research Center: Surface flow and heating distributions on a cylinder in near wake of Aeroassist Flight Experiment (AFE) configuration at incidence in Mach 10 air (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by William L. Wells (page images at HathiTrust)
• Langley Research Center: Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Barrett L. Shrout, Ida K. Collins, William A. Corlett, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Surface pressure measurements at two tips of a model helicopter rotor in hover (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by R. B. Gray and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Surface pressure measurements on a series of two-dimensional yawmeter bodies (National Aeronautics and Space Administration ;, 1976), also by M. J. Goodyer and University of Virginia. Research Laboratories for the Engineering Sciences (page images at HathiTrust)
• Langley Research Center: Surface recession characteristics of a cryogenic insulation subjected to arc-tunnel heating (National Aeronautics and Space Administration ;, 1975), also by C. M. Pittman and Ronald D. Brown (page images at HathiTrust)
• Langley Research Center: Survey of reader preferences concerning the format of NASA technical reports (National Aeronautics and Space Administration ;, 1982), also by Thomas E. Pinelli, Virginia M. Cordle, and Myron Glassman (page images at HathiTrust)
• Langley Research Center: A survey of structural material issues for a space station (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Jane A. Hagaman (page images at HathiTrust)
• Langley Research Center: Suspension systems for ground testing large space structures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Ronald R. Gold and Inc Dynamic Engineering (page images at HathiTrust)
• Langley Research Center: Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities (National Aeronautics and Space Administration ;, 1974), also by Milton Lamb and Robert L. Stallings (page images at HathiTrust)
• Langley Research Center: A swept wing panel in a low speed flexible walled test section (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987), also by M. J. Goodyer (page images at HathiTrust)
• Langley Research Center: Swing-Arm Beam Erector (SABER) concept for single astronaut assembly of space structure (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Judith J. Watson, J. Kermit Jensen, and Walter L. Heard (page images at HathiTrust)
• Langley Research Center: Symmetry considerations in the scattering of identical composite bodies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by John W. Norbury, Philip A. Deutchman, and Lawrence W. Townsend (page images at HathiTrust)
• Langley Research Center: A Synchronous strobed laser light sheet for rotor flow visualization (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Bradley D. Leighty (page images at HathiTrust)
• Langley Research Center: Synthetic Aperture Radar imagery of airports and surrounding areas : archived SAR data (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Robert G. Onstott, Denise J. Gineris, and Environmental Research Institute of Michigan (page images at HathiTrust)
• Langley Research Center: Synthetic Aperture Radar imagery of airports and surrounding areas : Denver Stapleton International Airport (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Robert G. Onstott, Denise J. Gineris, and Environmental Research Institute of Michigan (page images at HathiTrust)
• Langley Research Center: Synthetic Aperture Radar imagery of airports and surrounding areas : Philadalphia Airport (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Robert G. Onstott, Denise J. Gineris, and Environmental Research Institute of Michigan (page images at HathiTrust)
• Langley Research Center: Synthetic aperture radar imagery of airports and surrounding areas : study of clutter at grazing angles and their polarimetric properties (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Robert G. Onstott, James T. Clinthorne, Denise J. Gineris, and Environmental Research Institute of Michigan (page images at HathiTrust)
• Langley Research Center: A System for aerodynamic design and analysis of supersonic aircraft. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by R. G. Coleman, J. L. Lundry, W. D. Middleton, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A system for spacecraft attitude control and energy storage (National Aeronautics and Space Administration ;, 1974), also by J. D. Shaughnessy (page images at HathiTrust)
• Langley Research Center: System status display evaluation (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Leland G. Summers (page images at HathiTrust)
• Langley Research Center: Systematic study of error sources in supersonic skin-friction balance measurements (National Aeronautics and Space Administration ;, 1976), also by Jerry M. Allen and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A T-matrix theory of galactic heavy-ion fragmentation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by John W. Norbury, Philip A. Deutchman, and Lawrence W. Townsend (page images at HathiTrust)
• Langley Research Center: Table and charts of equilibrium normal shock and shock-tube properties for pure argon with velocities to 18 km/sec (Scientific and Technical Information Office, National Aeronautics and Space Administration ;, 1976), also by Charles G. Miller and Sue E. Wilder (page images at HathiTrust)
• Langley Research Center: Table and charts of equilibrium normal-shock and shock-tube properties for pure carbon dioxide with velocities from 1 to 16 km/sec (Scientific and Technical Information Office, National Aeronautics and Space Administration ;, 1976), also by Charles G. Miller and Sue E. Wilder (page images at HathiTrust)
• Langley Research Center: Tables and charts for estimating stall effects on lifting-rotor characteristics (National Aeronautics and Space Administration, 1960), also by Alfred Gessow and Robert J. Tapscott (page images at HathiTrust)
• Langley Research Center: Tables and charts of equilibrium thermodynamic properties of ammonia for temperatures from 500 to 50 000 K (Scientific and Technical Information Office, National Aeronautics and Space Administration ;, 1976), also by Ann L. Simmonds, John E. Nealy, and Charles G. Miller (page images at HathiTrust)
• Langley Research Center: Tables and charts of equilibrium thermodynamic properties of carbon dioxide for temperatures from 100 K to 25 000 K (Scientific and Technical Information Office, National Aeronautics and Space Administration ;, 1976), also by Charles G. Miller and Sue E. Wilder (page images at HathiTrust)
• Langley Research Center: Tables of aerodynamic coefficients obtained from developed Newtonian expressions for complete and partial conic and spheric bodies at combined angles of attack and sideslip with some comparisons with hypersonic experimental data (U.S. G.P.O., 1962), also by William R. Wells, William O. Armstrong, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Tables of Mie scattering functions for particles with refractive index 1.5 (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1969), also by Michael P. McCormick, James D. Lawrence, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Tabulated data from a pressure-distribution investigation at mach number 2.01 of the wing of a canard airplane model (National Aeronautics and Space Administration, 1959), also by Cornelius Driver and James L. Jacocks (page images at HathiTrust)
• Langley Research Center: A tabulation of helicopter rotor-blade differential pressures, stresses, and motions as measured in flight (National Aeronautics and Space Administration, 1964), also by James Scheiman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Take-off distances of a supersonic transport configuration as affected by airplane rotation during the take-off run (National Aeronautics and Space Administration, 1961), also by Albert W. Hall and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Target correlation effects on neutron-nucleus total, absorption, and abrasion cross sections (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Francis A. Cucinotta, John W. Wilson, and Lawrence W. Townsend (page images at HathiTrust)
• Langley Research Center: The TE01 mode reflection coefficient of a ground-plane mounted parallel-plate waveguide illuminating a reflecting sheet (National Aeronautics and Space Administration ;, 1969), also by L. L. Tsai, R. C. Rudduck, and Ohio State University (page images at HathiTrust)
• Langley Research Center: Technical communications in aeronautics : results of an exploratory study (National Aeronautics and Space Administration, Langley Research Center ;, 1989), also by Thomas E. Pinelli and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Technical communications in aeronautics : results of an exploratory study : an analysis of managers' and nonmanagers' responses (National Aeronautics and Space Administration, Langley Research Center ;, 1989), also by Thomas E. Pinelli and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Technical communications in aeronautics : results of an exploratory study : an analysis of profit managers' and nonprofit managers' responses (National Aeronautics and Space Administration, Langley Research Center ;, 1989), also by Thomas E. Pinelli and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A technique for designing active control systems for astronomical-telescope mirrors (National Aeronautics and Space Administration ;, 1973), also by W. E. Howell and J. F. Creedon (page images at HathiTrust)
• Langley Research Center: A technique for evaluating the application of the pin-level stuck-at fault model to VLSI circuits (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Daniel L. Palumbo and George B. Finelli (page images at HathiTrust)
• Langley Research Center: A technique for generating arbitrarily shaped curved approach paths (National Aeronautics and Space Administration ;, 1976), also by Walter J. McConnell and Sperry Flight Systems (Firm) (page images at HathiTrust)
• Langley Research Center: Technique for removal of angular momentum from a spacecraft momentum-exchange system by use of the gravity-gradient moments (National Aeronautics and Space Administration ;, 1966), also by David B. Middleton (page images at HathiTrust)
• Langley Research Center: A technique for thrust-vector orientation during manual control of lunar landings from a synchronous orbit (National Aeronautics and Space Administration :, 1964), also by L. Keith Barker and M. J. Queijo (page images at HathiTrust)
• Langley Research Center: A technique to infer atmospheric temperature from horizon radiance profiles (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal scientific and Technical Information, Springfield, Va., 1969), also by Thomas B. McKee, Jules J. Lambiotte, Ruth I. Whitman, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: A Technique to infer atmospheric water-vapor mixing ratio from measured horizon radiance profiles (National Aeronautics and Space Administration, 1969), also by Thomas B. McKee, Jules J. Lambiotte, Ruth I. Whitman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A technique using a nonlinear helicopter model for determining trims and derivatives (U.S. National Aeronautics and Space Administration ;, 1976), also by Aaron J. Ostroff, William J. Rood, David R. Downing, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Techniques for generation of control and guidance signals derived from optical fields : Part II (National Aeronautics and Space Administration :, 1971), also by H. Hemami, S. R. Gardner, R. B. McGhee, Ohio State University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Techniques for selection and analysis of parachute deployment systems (National Aeronautics and Space Administration ;, 1970), also by Earle K. Huckins (page images at HathiTrust)
• Langley Research Center: Technology for pressure-instrumented thin airfoil models (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by David A. Wigley (page images at HathiTrust)
• Langley Research Center: Technology requirements for advanced earth orbital transportation systems (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by A. K. Hepler, E. L. Bangsund, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Technology requirements for advanced earth-orbital transportation systems, duel-mode propulsion (National Aeronautics and Space Administration ;, 1977), also by Rudolph C. Haefeli, Martin Marietta Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Technology requirements for advanced earth-orbital transportation systems : summary report (National Aeronautics and Space Administration ;, 1977), also by Rudolph C. Haefeli, Martin Marietta Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Technology requirements for future Earth-to-geosynchronous orbit transportation systems. Volume 1, Executive summary (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Vincent A. Calouri, James C. Jenkins, Robert T. Conrad, and Boeing Aerospace Company (page images at HathiTrust)
• Langley Research Center: Temperature and composition of a plasma obtained by seeding a cyanogen-oxygen flame with cesium (National Aeronautics and Space Administration, 1960), also by Richard A. Hord and J. Byron Pennington (page images at HathiTrust)
• Langley Research Center: Temporal and spatial inconsistencies of time-split finite-difference schemes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Douglas L. Dwoyer, Frank C. Thames, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Tensile behavior of boron-filament-reinforced epoxy rings and belts (National Aeronautics and Space Administration ;, 1969), also by Robert M. Baucom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Tensile creep of boron/epoxy and boron/epoxy-reinforced 7075-T6 aluminum alloy (U.S. National Bureau of Standards :, 1972), also by Daniel J. Chwirut (page images at HathiTrust)
• Langley Research Center: Tensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ̊to 400 ̊F (370 ̊to 480 ̊K) (National Aeronautics and Space Administration ;, 1969), also by Dick M. Royster and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Tensile stress-strain behavior of graphite/epoxy laminates (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by D. P. Garber, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Kentron Technical Center (page images at HathiTrust)
• Langley Research Center: Tension, compression, and fatigue properties of several SAE 52100 and tool steels used for ball bearings (National Aeronautics and Space Administration, 1960), also by G. Sachs, V. Weiss, and R. Sell (page images at HathiTrust)
• Langley Research Center: Terminal area automatic navigation, guidance, and control research using the microwave landing system (MLS) : part 1, automatic rollout, turnoff, and taxi (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981), also by Samuel Pines and Analytical Mechanics Associates (page images at HathiTrust)
• Langley Research Center: Terminal area automatic navigation, guidance, and control research using the microwave landing system (MLS) part 4, transition path reconstruction along a straight line path containing a glideslope change waypoint (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982), also by Samuel Pines and Analytical Mechanics Associates (page images at HathiTrust)
• Langley Research Center: Terminal area automatic navigation, guidance, and control research using the microwave landing system (MLS) : part 2, RNAV/MLS transition problems for aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983), also by Samuel Pines and Analytical Mechanics Associates (page images at HathiTrust)
• Langley Research Center: Terminal area automatic navigation, guidance, and control research using the microwave landing system (MLS) : part 3, a comparison of waypoint guidance algorithms for RNAV/MLS transition (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982), also by Samuel Pines and Analytical Mechanics Associates (page images at HathiTrust)
• Langley Research Center: Terminal-area flight procedures and route design for supersonic transport New York-transatlantic operations (National Aeronautics and Space Administration ;, 1972), also by Richard H. Sawyer and Milton D. McLaughlin (page images at HathiTrust)
• Langley Research Center: Test and analysis of Celion 300/PMR-15, graphite/polyimide bonded composite joints : summary (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by J. B. Cushman, S. H. Ward, S. F. McCleskey, and Boeing Aerospace Company (page images at HathiTrust)
• Langley Research Center: Test and evaluation of the Generalized Gate Logic System Simulator (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Paul S. Miner (page images at HathiTrust)
• Langley Research Center: Test methods for textile composites (National Aeronautics and Space Administration, Langley Research Center ;, 1994), also by Pierre J. Minguet, Christian K. Gunther, and Mark J. Fedro (page images at HathiTrust)
• Langley Research Center: Test sections for small theoretical wind-tunnel-boundary interference on V/STOL models (National Aeronautics and Space Administration, 1968), also by Ray H. Wright and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Testing techniques for determining static mechanical properties of pneumatic tires (National Aeronautics and Space Administration ;, 1974), also by Richard N. Dodge and University of Michigan (page images at HathiTrust)
• Langley Research Center: Tests of graphite/polymide sandwich panels in uniaxial edgewise compression (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1980), also by Charles J. Camarda and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Tests on propellers under static thrust conditions (National Aeronautic and Space Administration ;, 1969), also by A. E. Brusse, C. F. Kettleborough, A. E. Cronk, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Texcad-- textile composite analysis for design : version 1.0 user's manual (National Aeronautics and Space Administration ;, 1994), also by Rajiv A. Naik and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Theorectical studies of compressor noise (National Aeronautics and Space Administration ;, 1969), also by M. V. Lowson, United States National Aeronautics and Space Administration, and Wyle Laboratories (page images at HathiTrust)
• Langley Research Center: Theoretical aerodynamics of upper-surface-blowing jet-wing interaction (National Aeronautics and Space Administration ;, 1975), also by C. Edward Lan and James F. Campbell (page images at HathiTrust)
• Langley Research Center: A theoretical analysis of airplane longitudinal stability and control as affected by wind shear (National Aeronautics and Space Administration ;, 1977), also by Windsor L. Sherman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A theoretical analysis of simulated transonic boundary layers in cryogenic-nitrogen wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Jerry B. Adcock, Charles B. Johnson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Theoretical analysis of the creep collapse of columns (National Aeronautics and Space Administration, 1959), also by Floyd R. Schlechte (page images at HathiTrust)
• Langley Research Center: A theoretical analysis of the free vibration of discretely stiffened cylindrical shells with arbitrary end conditions (National Aeronautics and Space Administration ;, 1969), also by D. M. Egle, K. E. Soder, University of Oklahoma, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Theoretical and experimental flow fields for a supersonic cruise fighter forebody (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Steven F. Yaros (page images at HathiTrust)
• Langley Research Center: A theoretical and experimental investigation of cylindrical electrostatic probes at arbitrary incidence in flowing plasma (National Aeronautics and Space Administration ;, 1974), also by Renaldo V. Jenkins and W. Linwood Jones (page images at HathiTrust)
• Langley Research Center: Theoretical and experimental investigation of ground-induced effects for a low-aspect-ratio highly swept arrow-wing configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Paul L. Coe, James L. Thomas, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Theoretical and experimental investigation of the performance of a fan-in-wing VTOL configuration (National Aeronautics and Space Administration ;, 1973), also by Harry H. Heyson (page images at HathiTrust)
• Langley Research Center: Theoretical and experimental longitudinal aerodynamic characteristics of an aspect ratio 0.25 sharp-edge delta wing at subsonic, supersonic, and hypersonic speeds (National Aeronautics and Space Administration ;, 1974), also by Charles H. Fox and John E. Lamar (page images at HathiTrust)
• Langley Research Center: Theoretical and experimental studies of reentry plasmas (National Aeronautics and Space Administration ;, 1973), also by M. G. Dunn, Sang-Wook Kang, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Langley Research Center: Theoretical and experimental study of a new method for prediction of profile drag of airfoil sections (National Aeronautics and Space Administration ;, 1975), also by Suresh H. Goradia, D. G. Lilley, and Lockheed-Georgia Company (page images at HathiTrust)
• Langley Research Center: Theoretical and experimental study of twisted and cambered delta wings designed for a mach number of 3.5 (National Aeronautics and Space Administration ;, 1976), also by Russell B. Sorrells, Emma Jean Landrum, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Theoretical comparison of beads, wires, and films as rocketsonde temperature sensors in the mesosphere (National Aeronautics and Space Administration ;, 1969), also by Forrest L. Staffanson, University of Utah, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Theoretical estimation of the transonic aerodynamic characteristics of a supercritical-wing transport model with trailing-edge controls (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by James M. Luckring, Michael J. Mann, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Theoretical evaluation of high-speed aerodynamics for arrow-wing configurations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Samuel M. Dollyhigh and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Theoretical flow field calculations for project ram (National Aeronautics and Space Administration ;, 1969), also by H. Webb and North American Rockwell Corporation (page images at HathiTrust)
• Langley Research Center: Theoretical frequency response functions and power spectra of the XB-70 response to atmospheric turbulence (National Aeronautics and Space Administration, 1970), also by Thomas E. Stenton, United States National Aeronautics and Space Administration, and North American Rockwell Corporation (page images at HathiTrust)
• Langley Research Center: A theoretical investigation of forebody shapes designed for natural laminar boundary-layer flow (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Raymond L. Barger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A theoretical investigation of noise reduction through the-cylindrical fuselage of a twin-engine, propeller-driven aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Rama B. Bhat, John S. Mixson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A theoretical investigation of simulation in expansion tubes and tunnels (National Aeronautics and Space Administration, 1966), also by Robert L. Trimpi and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A theoretical investigation of the input characteristics of a rectangular cavity-backed slot antenna (National Aeronautics and Space Administration ;, 1975), also by C. R. Cockrell (page images at HathiTrust)
• Langley Research Center: Theoretical method for deriving an earth-centered datum from optical observations of the earth's horizon from an earth satellite (National Aeronautics and Space Administration, 1966), also by Ruben L. Jones and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A theoretical method for the analysis and design of axisymmetric bodies (National Aeronautics and Space Administration ;, 1975), also by T. D. Beatty and McDonnell Douglas Corporation (page images at HathiTrust)
• Langley Research Center: Theoretical nitric oxide production incidental to autoignition and combustion of several fuels homogeneously dispersed in air under some typical hypersonic flight conditions (National Aeronautics and Space Administration, 1974), also by Gilbert S. Bahn, United States National Aeronautics and Space Administration, and LTV Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Theoretical prediction of nonlinear propagation effects on noise signatures generated by subconic or supersonic propeller - or rotor-blade tips (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Raymond L. Barger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Theoretical studies of radiation effects on composite materials for space use (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by C. Ken Chang, Efstathios Kamaratos, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Theoretical study of corrugated plates : shearing of a trapezoidally corrugated plate with through lines permitted to curve (National Aeronautics and Space Administration, 1971), also by Chuan-jui Lin, Charles Libove, United States. National Aeronautical and Space Administration, and Syracuse University (page images at HathiTrust)
• Langley Research Center: Theoretical study of nonadiabatic boundary-layer stabilization times in a cryogenic wind tunnel for typical stainless-steel wing and fuselage models (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Charles B. Johnson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: A theoretical study of radar return and radiometric emission from the sea (National Aeronautics and Space Administration ;, 1972), also by William H. Peake and Ohio State University (page images at HathiTrust)
• Langley Research Center: Theoretical study of reactive and nonreactive turbulent coaxial jets (U.S. National Aeronautics and Space Administration ;, 1976), also by Roop N. Gupta, N. T. Wakelyn, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Theoretical study of refraction effects on noise produced by turbulent jets (National Aeronautics and Space Administration ;, 1975), also by E. W. Graham, B. B. Graham, and Wash.) Graham Associates (Shaw Island (page images at HathiTrust)
• Langley Research Center: A Theoretical study of stagnation-point ablation (U.S. G.P.O., 1959), also by Leonard Roberts and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A theoretical study of the angular motions of spinning bodies in space (U.S. Government Printing Office, 1961), also by Jerrold H. Suddath and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Theoretical study of the effect of wind velocity gradients on longitudinal stability and control in climbing and level flight (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Windsor L. Sherman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Theoretical study of the effects of refraction on the noise produced by turbulence in jets (National Aeronautics and Space Administration ;, 1974), also by E. W. Graham, B. B. Graham, and Wash.) Graham Associates (Shaw Island (page images at HathiTrust)
• Langley Research Center: Theoretical study of the use of variable geometry in the design of minimal-correction V/STOL wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1969), also by Harry H. Heyson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Theory and apparatus for measurement of emissivity for radiative cooling of hypersonic aircraft with data for inconel, iconel X, stainless steel 303, and titanium alloy RS-120 (U.S. G.P.O., 1961), also by William J. O'Sullivan, William R. Wade, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Theory for computing the field scattered from a smooth inflected surface (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Raymond L. Barger and Allen K. Dominek (page images at HathiTrust)
• Langley Research Center: Theory for computing the size and shape of a region of influence associated with a maneuvering vehicle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Raymond L. Barger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A theory for predicting boundary impedance and resonance, frequencies of slotted-wall wind tunnels, including plenum effects (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Raymond L. Barger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Theory of an airfoil equipped with a jet flap under low-speed flight conditions (National Aeronautics and Space Administration ;, 1975), also by F. L. Addessio, J. G. Skifstad, and Purdue University. School of Mechanical Engineering (page images at HathiTrust)
• Langley Research Center: Theory of low transitions in CO discharge lasers (National Aeronautics and Space Administration ;, 1976), also by Barry D. Sidney and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Theory of noise generation from moving bodies with an application to helicopter rotors (National Aeronautics and Space Administration ;, 1975), also by F. Farassat (page images at HathiTrust)
• Langley Research Center: Thermal and aerothermal performance of titanium multiwall thermal protection system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Don E. Avery, John L. Shideler, Lyndon B. Johnson Space Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Thermal and structural tests of a hydrogen cooled panel (National Aeronautics and Space Administration ;, 1972), also by C. E. Richard and AiResearch Manufacturing Company of Los Angeles (Calif.) (page images at HathiTrust)
• Langley Research Center: Thermal design for areas of interference heating on actively cooled hypersonic aircraft (National Aeronautics and Space Administration, Scientific and Technical Office ;, 1978), also by R. L. Herring, J. E. Stone, McDonnell Douglas Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Thermal-distortion analysis of a spacecraft box truss in geostationary orbit (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Patrick A. Cosgrove, Lawrence F. Rowell, and Jeffery T. Farmer (page images at HathiTrust)
• Langley Research Center: Thermal-distortion analysis of an antenna strongback for geostationary high-frequency microwave applications (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Jeffery T. Farmer, Robert L. Wright, and Deborah M. Wahls (page images at HathiTrust)
• Langley Research Center: Thermal dynamic modeling study (National Aeronautics and Space Administration ;, 1972), also by I. U. Ojalvo and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Thermal stresses in coatings on carbon-carbon composites (National Aeronautics and Space Administration, Langley Research Center, 1996), also by Andreas W. Obst and M. W. Hyer (page images at HathiTrust)
• Langley Research Center: Thermal-structural combined loads design criteria study (National Aeronautics and Space Administration ;, 1972), also by V. Deriugin and Boeing Company (page images at HathiTrust)
• Langley Research Center: Thermal-structural design study of an airframe-integrated scramjet : summary report (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by O. A. Buchmann and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Thermodynamic and transport properties of gaseous tetrafluoromethane in chemical equilibrium (National Aeronautics and Space Administration ;, 1973), also by James L. Hunt and Lillian R. Boney (page images at HathiTrust)
• Langley Research Center: Thermodynamic properties of gaseous fluorocarbons and isentropic equilibrium expansions of two binary mixtures of fluorocarbons and argon (National Aeronautics and Space Administration ;, 1977), also by Noel A. Talcott and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Thermodynamic properties of hydrogen-helium plasmas (National Aeronautics and Space Administration ;, 1971), also by H. F. Nelson and University of Missouri--Rolla. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• Langley Research Center: Thermodynamic, transport, and flow properties of gaseous products resulting from combustion of methane-air-oxygen mixtures (National Aeronautics and Space Administration ;, 1976), also by George F. Klieb and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Thermoelastic damping and its effect on flutter of stressed panels situated in a supersonic airflow (National Aeronautics and Space Administration ;, 1971), also by R. C. Shieh and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Thermomechanical processing of Haynes alloy no. 188 sheet to improve creep strength (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978), also by D. L. Klarstrom and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Thin film oxygen partial pressure sensor (National Aeronautics and Space Administration ;, 1972), also by J. J. Wortman and Research Triangle Institute (page images at HathiTrust)
• Langley Research Center: Third-order contributions to electrical conduction in plasmas (National Aeronautics and Space Administration ;, 1969), also by Willard E. Meador and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Three-deminsional finite-element analysis of finite-thickness fracture specimens (National Aeronautics and Space Administration ;, 1977), also by I. S. Raju, J. C. Newman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A three-dimensional analysis of the effects of heat generation in plates (National Aeronautics and Space Administration ;, 1968), also by Robert R. McWithey (page images at HathiTrust)
• Langley Research Center: Three-dimensional boundary-layer program (BL3D) for swept subsonic or supersonic wings with application to laminar flow control (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), also by Venkit Iyer and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Langley Research Center: Three-dimensional cavity flow fields at subsonic and transonic speeds (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by E. B. Plentovich (page images at HathiTrust)
• Langley Research Center: Three-dimensional transonic potential flow about complex three-dimensional configurations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Theodore A. Reyhner, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Three input concepts for flight crew interaction with information presented on a large-screen electronic cockpit display (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Denise R. Jones (page images at HathiTrust)
• Langley Research Center: Three-track runway and taxiway profiles measured at international airports A and B (National Aeronautics and Space Administration :, 1969), also by Albert W. Hall and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Three-track runway and taxiway profiles measured at international airports E and F (National Aeronautics and Space Administration ;, 1971), also by Albert W. Hall and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Three-track runway and taxiway profiles measured at international airports G and H (National Aeronautics and Space Administration, 1972), also by Albert W. Hall and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Three-track runway and taxiway profiles measured at international airports I and J (National Aeronautics and Space Administration ;, 1972), also by Albert W. Hall (page images at HathiTrust)
• Langley Research Center: Three-track runway elevation profiles measured at two United States government installations (National Aeronautics and Space Administration ;, 1969), also by Garland J. Morris and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Thrusting trajectory minimization program for orbital transfer maneuvers (National Aeronautics and Space Administration, 1971), also by Lawrence H. Hoffman, George R. Young, Richard N. Green, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Michael J. Bockelie and Peter R. Eiseman (page images at HathiTrust)
• Langley Research Center: Time and temperature dependent modulus of Pyrrone and polyimide moldings (National Aeronautics and Space Administration ;, 1972), also by L. L. Lander and Avco Corporation. Systems Division (page images at HathiTrust)
• Langley Research Center: Time-asymptotic solutions of the Navier-Stokes equations for free shear flows using an alternating-direction implicit method (National Aeronautics and Space Administration ;, 1976), also by David H. Rudy, Dana J. Morris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Time-critical multirate scheduling using contemporary real-time operating system services (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Dave E. Eckhardt and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Time-domain finite elements in optimal control with application to launch-vehicle guidance (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Robert R. Bless and Georgia Institute of Technology. School of Aerospace Engineering (page images at HathiTrust)
• Langley Research Center: Time-fixed rendezvous by impulse factoring with an intermediate timing constraint (National Aeronautics and Space Administration ;, 1974), also by Richard N. Green, George R. Young, and James F. Kibler (page images at HathiTrust)
• Langley Research Center: Time history solution program, L225 (TEV126). (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by R. E. Clemmons, A. Tornallyay, R. I. Kroll, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Tire stiffness and damping determined from static and free-vibration tests (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Robert K. Sleeper, Robert C. Dreher, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Tire tread temperatures during antiskid braking and cornering on a dry runway (National Aeronautics and Space Administration,Scientific and Technical Information Office ;, 1982), also by John A. Tanner and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: TM surface wave diffraction by a truncated dielectric slab recessed in a perfectly conducting surface (National Aeronautics and Space Administration, 1974), also by P. H. Pathak, R. G. Kouyoumjian, and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• Langley Research Center: Tools for embedded computing systems software. (National Aeronautics and Space administration, Scientific and Technical Information Office, 1978), also by American Institute of Aeronautics and Astronautics and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Torsion pendulum measurements on viscoelastic materials during vacuum exposure (National Aeronautics and Space Administration ;, 1972), also by Thomas C. Ward, Morris L. Evans, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Langley Research Center: Total energy-rate feedback for automatic glide-slope tracking during wind-shear penetration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Christine M. Belcastro and Aaron J. Ostroff (page images at HathiTrust)
• Langley Research Center: Trajectory control for vehicles entering the earth's atmosphere at small flight-path angles (U.S. G.P.O., 1961), also by John M. Eggleston, John W. Young, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Trajectory fitting in function space with application to analytic modeling of surfaces (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Raymond L. Barger (page images at HathiTrust)
• Langley Research Center: TRANDESNF : a computer program for transonic airfoil design and analysis in nonuniform flow (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987), also by Jen-Fu Chang and C. Edward Lan (page images at HathiTrust)
• Langley Research Center: A transformation method for constrained-function minimization (National Aeronautics and Space Administration ;, 1975), also by Stephen Keith Park (page images at HathiTrust)
• Langley Research Center: A transformation method for deriving, from a photograph, position and heading of a vehicle in a plane (National Aeronautics and Space Administration ;, 1976), also by Robert K. Sleeper, Eunice G. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: The transient response of coupled acousto-mechanical systems (National Aeronautics and Space Administration ;, 1969), also by A. Craggs and University of Southampton (page images at HathiTrust)
• Langley Research Center: Transient response of shells of revolution by direct integration and modal superposition methods (National Aeronautics and Space Administration ;, 1974), also by Wendell B. Stephens and Howard M. Adelman (page images at HathiTrust)
• Langley Research Center: Transition fixing for hypersonic flow (National Aeronautics and Space Administration ;, 1967), also by James R. Sterrett (page images at HathiTrust)
• Langley Research Center: Transitional boundary-layer solutions using a mixing-length and a two-equation turbulence model (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by E. Clay Anderson, David C. Wilcox, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Transmission of 2.43 MeV electrons through thick silicon targets (National Aeronautics and Space Administration ;, 1969), also by Jag J. Singh and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Transonic aerodynamic and buffet characteristics of a packaged space station in combination with a Saturn V launch vehicle (National Aeronautics and Space Administration ;, 1964), also by C. Robert Carter (page images at HathiTrust)
• Langley Research Center: Transonic aerodynamic characteristics of a proposed assured crew return capability (ACRC) lifting-body configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by George M. Ware (page images at HathiTrust)
• Langley Research Center: Transonic aerodynamic characteristics of a tailless fixed-wing supersonic transport model (National Aeronautics and Space Administration ;, 1966), also by Edward J. Ray and Robert T. Taylor (page images at HathiTrust)
• Langley Research Center: Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location (National Aeronautics and Space Administration, 1960), also by Ralph P. Bielat and P. Kenneth Pierpont (page images at HathiTrust)
• Langley Research Center: The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack (National Aeronautics and Space Administration, 1960), also by Ralph P. Bielat, William J. Alford, and A. Warner Robins (page images at HathiTrust)
• Langley Research Center: Transonic aerodynamic loading characteristics of a wing-body-tail combination having 52.5° sweptback wing of aspect ratio 3 with conical wing camber and body indentation for a design Mach number [square root of] 2 (National Aeronautics and Space Administration, 1961), also by Marlowe D. Cassetti, William B. Igoe, Richard J. Re, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Transonic aeroelastic analysis of launch vehicle configurations (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by João Luiz Filgueiras de Azevedo (page images at HathiTrust)
• Langley Research Center: Transonic airfoil flowfield analysis using Cartesian coordinates (National Aeronautics and Space Administration ;, 1975), also by Leland A. Carlson and Texas A. and M. Research Foundation (page images at HathiTrust)
• Langley Research Center: Transonic and supersonic ejection release characteristics of six dynamically scaled external-store shapes from an 0.086-scale model of a current fighter airplane (National Aeronautics and Space Administration, 1959), also by William F. Hinson (page images at HathiTrust)
• Langley Research Center: Transonic and supersonic flutter trend investigation of a variable-sweep wing (National Aeronautics and Space Administration, 1961), also by John C. Stonesifer and Robert C. Goetz (page images at HathiTrust)
• Langley Research Center: Transonic flutter investigation of models of proposed horizontal tails for the X-15 airplane (National Aeronautics and Space Administration, 1961), also by Lou S. Young (page images at HathiTrust)
• Langley Research Center: Transonic flutter investigation of models of the X-15 airplane horizontal tail (National Aeronautics and Space Administration, 1961), also by Lou S. Young and Samuel R. Bland (page images at HathiTrust)
• Langley Research Center: Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles (National Aeronautics and Space Administration ;, 1974), also by M. C. Sandford, Irving Abel, and Charles L. Ruhlin (page images at HathiTrust)
• Langley Research Center: A transonic interactive boundary-layer theory for laminar and turbulent flow over swept wings (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Shawn H. Woodson and Fred R. DeJarnette (page images at HathiTrust)
• Langley Research Center: A transonic investigation of base pressures associated with shallow three-dimensional rearward-facing steps (National Aeronautics and Space Administration ;, 1965), also by Thomas C. Kelly (page images at HathiTrust)
• Langley Research Center: Transonic Navier-Stokes calculations about a 65⁰ delta wing (National Aeronautics and Space Administration, Langley Research Center ;, 1994), also by W. Kelly Londenberg (page images at HathiTrust)
• Langley Research Center: Transonic Navier-Stokes solutions of three-dimensional afterbody flows (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by William B. Compton (page images at HathiTrust)
• Langley Research Center: Transonic pressure and load distributions for a group of simulated launch vehicles (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Thomas C. Kelly and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Transonic pressure measurements and comparison of theory to experiment for an arrow-wing configuration (National Aeronautics and Space Administration ;, 1976), also by Marjorie E. Manro and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: Transonic pressure measurements and comparison of theory to experiment for three arrow-wing configurations : summary report (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Marjorie E. Manro and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A transonic-small-disturbance wing design methodology (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Pamela S. Phillips, Richard L. Campbell, and Edgar G. Waggoner (page images at HathiTrust)
• Langley Research Center: Transonic wind-tunnel investigation of the effect of control span and large wing-tip nacelles on effectiveness of spoiler-slot-deflector controls on an unswept-wing fighter-type airplane (National Aeronautics and Space Administration, 1960), also by Dewey E. Wornom (page images at HathiTrust)
• Langley Research Center: Transonic wind-tunnel investigation of the fin loads of a 1/8-scale model simulating the first stage of the Scout research vehicle (National Aeronautics and Space Administration, 1961), also by Thomas C. Kelly (page images at HathiTrust)
• Langley Research Center: Transonic wind-tunnel investigation of the static aerodynamic characteristics of several configurations of the Blue Scout launch vehicle (National Aeronautics and Space Administration, 1963), also by Thomas C. Kelly and Robert J. Keynton (page images at HathiTrust)
• Langley Research Center: A transonic wind-tunnel investigation of the static longitudinal and lateral aerodynamic characteristics of a proposed hypersonic glider with several booster configurations (National Aeronautics and Space Administration, 1960), also by Ralph P. Bielat and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Transonic wind-tunnel tests of an error-compensated static-pressure probe (National Aeronautics and Space Administration, 1961), also by Francis J. Capone and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Transport methods and interactions for space radiations (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by John W. Wilson (page images at HathiTrust)
• Langley Research Center: Transport properties at high temperatures of CO₂-N₂-O₂-Ar gas mixtures for planetary entry applications (National Aeronautics and Space Administration ;, 1969), also by Jerry S. Lee, Percy J. Bobbitt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Transportation and handling loads. (National Aeronautics and Space Administration;, 1971), also by F. E. Ostrem (page images at HathiTrust)
• Langley Research Center: Trends in repeated loads on transport airplanes (National Aeronautics and Space Administration ;, 1968), also by Thomas L. Coleman (page images at HathiTrust)
• Langley Research Center: A triangular thin shell finite element : linear analysis (National Aeronautics and Space Administration ;, 1975), also by G. R. Thomas, Richard H. Gallagher, and Cornell University (page images at HathiTrust)
• Langley Research Center: A triangular thin shell finite element : nonlinear analysis (National Aeronautics and Space Administration ;, 1975), also by G. R. Thomas, Richard H. Gallagher, and Cornell University (page images at HathiTrust)
• Langley Research Center: Triangulation of multistation camera data to locate a curved line in space (National Aeronautics and Space Administration ;, 1974), also by Clifford L. Fricke (page images at HathiTrust)
• Langley Research Center: Turbojet-engine noise studies to evaluate effects of inlet-guide-vane--rotor spacing (National Aeronautics and Space Administration, 1968), also by John L. Crigler, Garland J. Morris, W. Latham Copeland, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Turbulent boundary layer over solid and porous surfaces with small roughness (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Fred Y. Kong, Fayette Collier, Joseph A. Schetz, Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Turbulent-flow separation criteria for overexpanded supersonic nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by E. Leon Morrisette, Theodore J. Goldberg, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Turbulent heat-transfer prediction method for application to scramjet engines (National Aeronautics and Space Administration ;, 1974), also by S. Z. Pinckney (page images at HathiTrust)
• Langley Research Center: Turbulent mixing of coaxial compressible hydrogen-air jets (National Aeronautics and Space Administration :, 1971), also by James M. Eggers and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Turbulent wall jet in a coflowing stream (National Aeronautics and Space Administration ;, 1975), also by James F. Campbell (page images at HathiTrust)
• Langley Research Center: A tutorial on the CARE III approach to reliability modeling (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Kishor Shridharbhai Trivedi, Robert M. Geist, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Two bonded half planes with a crack going through the interface (National Aeronautics and Space Administration ;, 1973), also by F. Erdogan, V. Biricikoglu, and Lehigh University (page images at HathiTrust)
• Langley Research Center: A two dimensional, iterative solution for the jet flap (National Aeronautics and Space Administration ;, 1973), also by Alan Charles Herold and University of Washington (page images at HathiTrust)
• Langley Research Center: Two-dimensional stability of laminar flames (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by H. S. Mukunda and J. Philip Drummond (page images at HathiTrust)
• Langley Research Center: Two-dimensional wind tunnel test of an oscillating rotor airfoil, volume II (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by L. U. Dadone, Boeing Vertol Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Two gas atmosphere sensor system (mass spectrometer) : phases IIa and IIb : prepared under contract no. NAS1-6387 for Langley Research Center (National Aeronautics and Space Administration ;, 1970), also by Perkin-Elmer Corporation (page images at HathiTrust)
• Langley Research Center: Two-impulse reorientation of asymmetric spacecraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by C. William Martz and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A two-parameter scintillation spectrometer system for measurement of secondary proton, deuteron, and triton distributions from materials under 558-MeV-proton irradiation (National Aeronautics and Space Administration ;, 1975), also by Sherwin M. Beck (page images at HathiTrust)
• Langley Research Center: A two-scale scattering model with application to the JONSWAP '75 Aircraft Microwave Scatterometer Experiment (National Aeronautics and Space Administration ;, 1977), also by Frank J. Wentz (page images at HathiTrust)
• Langley Research Center: Ultimate boundedness stability and controllability of hereditary systems (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Ethelbert N. Chukwu and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Ultrasonic signal enhancement by resonator techniques (National Aeronautics and Space Administration ;, 1973), also by Joseph S. Heyman (page images at HathiTrust)
• Langley Research Center: A unified acquisition system for acoustic data (National Aeronautics and Space Administration ;, 1977), also by Allan J. Zuckerwar, Harlan K. Holmes, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A unified development of several techniques for the representation of random vectors and data sets (National Aeronautics and Space Administration ;, 1973), also by W. Thomas Bundick (page images at HathiTrust)
• Langley Research Center: A unique facility for V/STOL aircraft hover testing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Richard G. Culpepper, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and United States. Naval Air Systems Command (page images at HathiTrust)
• Langley Research Center: An unsteady helicopter rotor : fuselage interaction analysis (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Peter F. Lorber, T. Alan Egolf, and United States. Army Aerostructures Directorate (page images at HathiTrust)
• Langley Research Center: Unsteady potential flow past a propeller blade section (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Mohammad Ali Takallu and Lockheed Engineering & Sciences Company (page images at HathiTrust)
• Langley Research Center: Upper-surface blowing nacelle design study for a swept wing airplane at cruise conditions (National Aeronautics and Space Administration ;, 1974), also by W. B. Gillette and Boeing Commercial Airplane Company (page images at HathiTrust)
• Langley Research Center: An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Peter A. Gnoffo (page images at HathiTrust)
• Langley Research Center: An upwind-biased space marching algorithm for supersonic viscous flow (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Francis A. Greene (page images at HathiTrust)
• Langley Research Center: U.S. standard atmospheres, 1962 : ICAO Standard atmosphere to 20 kilometers, proposed ICAO extension to 32 kilometers, tables and data to 700 kilometers. (U.S. Govt. print. off., 1963), also by United States. Committee on Extension to the Standard Atmosphere, United States National Aeronautics and Space Administration, United States. Weather Bureau, and United States Air Force (page images at HathiTrust)
• Langley Research Center: Use of a single turning vane to eliminate flow separation in a space-limited 90° intake elbow of an axial-flow compressor (National Aeronautics and Space Administration ;, 1965), also by S. Z. Pinckney (page images at HathiTrust)
• Langley Research Center: The use of coherence functions to determine dynamic excitation sources on launch vehicle payloads (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1979), also by Stanley Barrett, Robert M. Halvorson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: The use of computer-generated color graphic images for transient thermal analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by C. L. W. Edwards, James B. Hall, Frances T. Meissner, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Use of constrained optimization in the conceptual design of a medium-range subsonic transport (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Steven M. Sliwa and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Use of hexafluoroethane to simulate the inviscid real-gas effects on blunt entry vehicles (National Aeronautics and Space Administration ;, 1974), also by James L. Hunt, Kathryn A. Smith, and Robert A. Jones (page images at HathiTrust)
• Langley Research Center: The use of interactive graphic displays for interpretation of surface design parameters (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Noel A. Talcott and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Use of sensitivity analysis to predict performance as a function of different displays (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Michael L. Mout, George H. Burgin, Michael J. Walsh, inc Decision Science, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: User document for computer programs for ring-stiffened shells of revolution (National Aeronautics and Space Administration ;, 1973), also by Gerald A. Cohen and Structures Research Associates (page images at HathiTrust)
• Langley Research Center: User evaluation of ride technology research (National Aeronautics and Space Administration ;, 1976), also by J. R. McKenzie, Stanley H. Brumaghim, and Boeing Company. Wichita Division (page images at HathiTrust)
• Langley Research Center: User modeling techniques for enhanced usability of OPSMODEL operations simulation software (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by William T. Davis (page images at HathiTrust)
• Langley Research Center: User's guide for vectorized code EQUIL for calculating equilibrium chemistry on Control Data STAR-100 computer / Ajay Kumar, Randolph A. Graves, Jr., and K. James Weilmuenster. (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Ajay Kumar, K. James Weilmuenster, Randolph A. Graves, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: User's manual for a computer program to calculate discrete frequency noise of convention and advanced propellers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by R. M. Martin, F. Farassat, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Users' manual for the Langley high speed propeller noise prediction program (DFP-ATP) (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1989), also by M. H. Dunn and G. M. Tarkenton (page images at HathiTrust)
• Langley Research Center: User's manual for the One-Dimensional Hypersonic Experimental Aero-Thermodynamic (1DHEAT) data reduction code (National Aeronautics and Space Administration, Langley Research Center ;, 1995), also by Brian R. Hollis and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• Langley Research Center: Using minimal spanning trees to compare the reliability of network topologies (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Karen J. Leister, Kelly J. Hayhurst, and Allan L. White (page images at HathiTrust)
• Langley Research Center: USSAERO computer program development, versions B and C (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by F. A. Woodward and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Vacuum ultraviolet spectra of uranium hexafluoride/argon mixtures (U.S. National Aeronautics and Space Administration ;, 1976), also by N. L. Krascella and United Technologies Research Center (page images at HathiTrust)
• Langley Research Center: Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Harry W. Carlson, Michael J. Mann, and Christine M. Darden (page images at HathiTrust)
• Langley Research Center: Validation of an active gear, flexible aircraft take-off and landing analysis (AGFATL) (Langley Research Center, 1984), also by John R. McGehee (page images at HathiTrust)
• Langley Research Center: Validation of scramjet exhaust simulation technique (National Aeronautics and Space Administration ;, 1976), also by H. B. Hopkins, J. Leng, H. B. Konopka, United States National Aeronautics and Space Administration, and Grumman Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Validation of scramjet exhaust simulation technique at Mach 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by H. B. Hopkins, J. Leng, W. Konopka, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Validation of three-dimensional incompressible spatial direct numerical simulation code : a comparison with linear stability and parabolic stability equation theories for boundary-layer transition on a flat plate (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Ronald D. Joslin, Craig L. Streett, and Chau-Lyan Chang (page images at HathiTrust)
• Langley Research Center: Vapor-screen technique for flow visualization in the Langley Unitary Plan Wind Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Odell A. Morris (page images at HathiTrust)
• Langley Research Center: Vaporization and decomposition kinetics of candidate re-entry blackout suppressants in low-pressure flames (National Aeronautics and Space Administration ;, 1969), also by Shelby C. Kurzius, Fredrik H. Raab, and AeroChem Research Laboratories (page images at HathiTrust)
• Langley Research Center: The variation and control of range traveled in the atmosphere by a high-drag variable-lift entry vehicle (National Aeronautics and Space Administration, 1960), also by Donald C. Cheatham, John M. Eggleston, and John W. Young (page images at HathiTrust)
• Langley Research Center: A variational principle for compressible fluid mechanics : discussion of the multi-dimensional theory (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Robert Joel Prozan, Inc Continuum, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Vectorial reflectance of the Explorer IX satellite material (National Aeronautics and Space Administration, 1964), also by Gerald M. Keating, James A. Mullins, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Vectorization on the STAR computer of several numerical methods for a fluid flow problem (National Aeronautics and Space Administration ;, 1974), also by Jules J. Lambiotte and Lona M. Howser (page images at HathiTrust)
• Langley Research Center: Vehicle attitude determination with a single onboard camera (National Aeronautics and Space Administration ;, 1968), also by Richard J. Bendura, Robert E. Smith, and Allen B. Henning (page images at HathiTrust)
• Langley Research Center: Vehicle design considerations for active control application to subsonic transport aircraft (National Aeronautics and Space Administration ;, 1974), also by L. G. Hofmann, Warren F. Clement, McDonnell Douglas Astronautics Company-West, and inc Systems Technology (page images at HathiTrust)
• Langley Research Center: Velocity field of a round jet in a cross flow for various jet injection angles and velocity ratios (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Richard L. Fearn, Robert P. Weston, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Velocity measurements in the Langley 1-foot (0.305-meter) hypersonic arc tunnel (National Aeronautics and Space Administration ;, 1966), also by Roy James Duckett and Daniel I. Sebacher (page images at HathiTrust)
• Langley Research Center: Velocity-split Navier-Stokes solution procedure for imcompressible high Reynolds number external flows (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Douglas L. Dwoyer and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Venturi air-jet vacuum ejectors for high-volume atmospheric sampling on aircraft platforms (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Gerald Franklin Hill (page images at HathiTrust)
• Langley Research Center: Venusian atmospheric and Magellan properties from attitude control data (National Aeronautics and Space Administration, Langley Research Center, 1994), also by Christopher A. Croom and Robert H. Tolson (page images at HathiTrust)
• Langley Research Center: Verification of the FtCayuga fault-tolerant microprocessor system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Mandayam Srivas, Mark Bickford, and ORA Corporation (page images at HathiTrust)
• Langley Research Center: Vertical and lateral stiffness characteristics of aircraft tires (National Aeronautics and Space Administration ;, 1969), also by G. H. Nybakken, Samuel K. Clark, and Ohio State University (page images at HathiTrust)
• Langley Research Center: Vibration characteristics of 1/8-scale dynamic models of the space-shuttle solid-rocket boosters (National Aeronautics and Space Administration ;, 1976), also by Sumner A. Leadbetter and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Vibration characteristics of a cylinder partially filled with liquid with an attached elastic drain pipe (National Aeronautics and Space Administration ;, 1970), also by Robert J. Kroll and University of Cincinnati (page images at HathiTrust)
• Langley Research Center: Vibration characteristics of a steadily rotating slender ring (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Frederick J. Lallman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Vibration characteristics of walls and a plate glass window representative of those of a wood-frame house (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979), also by Huey D. Carden and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Vibration of skewed cantilever plates and helicoidal shells (National Aeronatics and Space Administration, 1975), also by D. P. Beres, C. D. Bailey, and Ohio State University (page images at HathiTrust)
• Langley Research Center: Vibrations measured in the passenger cabins of two jet transport aircraft (National Aeronautics and Space Administration ;, 1975), also by John J. Catherines, Harland F. Scholl, and John S. Mixon (page images at HathiTrust)
• Langley Research Center: Vibroacoustic response of structures and perturbation Reynolds stress near structure-turbulence interface (National Aeronautics and Space Administration ;, 1977), also by S. Maekawa, Y. K. Lin, University of Illinois at Urbana-Champaign, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Video camera system for locating bullet holes in targets at a ballistics range (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by A. W. Burner, W. K. Goad, and D. R. Rummler (page images at HathiTrust)
• Langley Research Center: Viking dynamics experience with application to future payload design (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Stanley Barrett, Kenneth R. Payne, W. Paul Rader, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Martin Marietta Corporation (page images at HathiTrust)
• Langley Research Center: Viking-Mars, anatomy of success (National Aeronuatics and Space Administration, Langley Research Center, 1978), also by Jet Propulsion Laboratory (U.S.) (page images at HathiTrust; US access only)
• Langley Research Center: Viking Mars mission support investigations in the Langley Transonic Dynamics Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Jerome T. Foughner and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Viscous computations of cold air/air flow around scramjet nozzle afterbody (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by Oktay Baysal, Walter C. Englelund, and Old Dominion University. Dept. of Mechanical Engineering and Mechanics (page images at HathiTrust)
• Langley Research Center: A viscous flow analysis for the tip vortex generation process (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by S.J. Shamroth, W. R. Briley, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Viscous-inviscid calculations of jet entrainment effects on the subsonic flow over nozzle afterbodies (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Richard G. Wilmoth and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Viscous theory of surface noise interaction phenomena (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by John E. Yates and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: The visual acuity in viewing scaled objects on television compared with that in direct viewing (National Aeronautics and Space Administration ;, 1969), also by Edward R. Long, Sheila Ann T. Long, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Visual aspects of a full-size pilot-controlled simulation of the Gemini-Agena docking (National Aeronautics and Space Administration :, 1965), also by Jack E. Pennington (page images at HathiTrust)
• Langley Research Center: Visual scanning behavior and pilot workload (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by J. R. Tole, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Massachusetts Institute of Technology (page images at HathiTrust)
• Langley Research Center: A visual technique for determining qualitative aerodynamic heating rates on complex configurations (National Aeronautics and Space Administration :, 1960), also by P. Calvin Stainback (page images at HathiTrust)
• Langley Research Center: Voice measures of workload in the advanced flight deck (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Sid J. Schneider, Richard O'Donnell, Murray Alpert, and Behavioral Health Systems (page images at HathiTrust)
• Langley Research Center: Voice measures of workload in the advanced flight deck : additional studies (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Sid J. Schneider, Murray Alpert, and Behavioral Health Systems (page images at HathiTrust)
• Langley Research Center: Voltage-programed control of turboalternator load (National Aeronautics and Space Administration, 1971), also by Richard N. Young, Eugene L. Kelsey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Volume, Area and Mass Properties : a computer program for calculating volume, area, and mass properties of aerospace vehicles (National Aeronautics and Space Administration ;, 1974), also by P. J. Norton, C. R. Glatt, and Aerophysics Research Corporation (page images at HathiTrust)
• Langley Research Center: Vortex equations : singularities, numerical solution, and axisymmetric vortex breakdown (National Aeronautics and Space Administration ;, 1972), also by Hartmut H. Bossel and Santa Barbara University of California (page images at HathiTrust)
• Langley Research Center: The vortex lattice method for the rotor-vortex interaction problem (National Aeronautics and Space Administration ;, 1974), also by Raghuveera Padakannaya and Pennsylvania State University (page images at HathiTrust)
• Langley Research Center: Vortex-lattice utilization : a workshop held at Langley Research Center, Hampton, Virginia, on May 17-18, 1976 (Scientific and Technical Information Office, National Aeronautics and Space Administration ;, 1976), also by Langley Research Center Vortex-Lattice Utilization Workshop (page images at HathiTrust)
• Langley Research Center: Wake analysis for supersonic decelerator applications (National Aeronautics and Space Administration ;, 1970), also by Richard A. Lau and Goodyear Aerospace Corporation (page images at HathiTrust)
• Langley Research Center: Wake geometry effects on rotor blade-vortex interaction noise directivity (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by R. M. Martin (page images at HathiTrust)
• Langley Research Center: Wake-shock interaction at a Mach number of 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Michael J. Walsh and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Lawrence L. Green and Perry A. Newman (page images at HathiTrust)
• Langley Research Center: Water landing characteristics of a model of a winged reentry vehicle (National Aeronautics and Space Administration ;, 1972), also by Sandy M. Stubbs (page images at HathiTrust)
• Langley Research Center: Water pressures and accelerations during landing of a dynamic model of the Apollo spacecraft with a deployed-heat-shield impact-attenuation system (National Aeronautics and Space Administration ;, 1968), also by Sandy M. Stubbs (page images at HathiTrust)
• Langley Research Center: Water-tunnel and analytical investigation of the effect of strake design variables on strake vortex breakdown characteristics (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Neal T. Frink, John E. Lamar, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Water-tunnel investigation of concepts for alleviation of adverse inlet spillage interactions with external stores (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Dan H. Neuhart and Matthew N. Rhode (page images at HathiTrust)
• Langley Research Center: A wave-envelope analysis of sound propagation in nonuniform circular ducts with compressible mean flows (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Ali Hasan Nayfeh, B. S. Shaker, John E. Kaiser, Virginia Polytechnic Institute and State University, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Wave theory of turbulence in compressible media (U.S. National Aeronautics and Space Administration ;, 1976), also by Czeslaw P. Kentzer, United States National Aeronautics and Space Administration, and Purdue University (page images at HathiTrust)
• Langley Research Center: Weak incident shock interactions with Mach 8 laminar boundary layers (National Aeronautics and Space Administration ;, 1974), also by Louis G. Kaufman and Charles B. Johnson (page images at HathiTrust)
• Langley Research Center: A weakly nonlinear theory for wave-vortex interactions in curved channel flow (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Bart A. Singer, Thomas A. Zang, and Gordon Erlebacher (page images at HathiTrust)
• Langley Research Center: Wear and related characteristics of an aircraft tire during braking (National Aeronautics and Space Administration ;, 1972), also by John L. McCarty (page images at HathiTrust)
• Langley Research Center: Wear, friction, and temperature characteristics of an aircraft tire undergoing braking and cornering (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by John L. McCarty, S. R. Riccitiello, Thomas J. Yager, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: The wedge hot-film anemometer in supersonic flow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by John M. Seiner and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: WIDOWAC (Wing Design Optimization with Aeroelastic Constraints) : program manual (National Aeronautics and Space Administration ;, 1974), also by Raphael T. Haftka and James H. Starnes (page images at HathiTrust)
• Langley Research Center: A wind-compensation method and results of its application to flight tests of twelve trailblazer rocket vehicles (National Aeronautics and Space Administration, 1964), also by Allen B. Henning, Jean C. Keating, Reginald R. Lundstrom, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind data from the 250-foot (76.2-meter) tower at Wallops Island, Virginia (National Aeronautics and Space Administration, 1968), also by James A. Cochrane, Robert M. Henry, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind loads on vertically launched vehicles at various geographic locations and launch altitudes (National Aeronautics and Space Administration, 1966), also by Robert M. Henry, James A. Cochrane, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Langley Research Center: Wind-tunnel buffeting measurements on two wing end-plate airplane model configurations (National Aeronautics and Space Administration ;, 1967), also by William B. Igoe (page images at HathiTrust)
• Langley Research Center: Wind-tunnel experiments on divergence of forward-swept wings (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Rodney H. Ricketts, Robert V. Doggett, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Emma Jean Landrum, C. Donald Babb, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Wind tunnel free flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Long P. Yip (page images at HathiTrust)
• Langley Research Center: Wind tunnel interference factors for high-lift wings in closed wind tunnels (National Aeronautics and Space Administration, 1973), also by Robert G. Joppa and University of Washington (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation at a Mach number of 2.91 of stability and control characteristics of three lifting reentry configurations at angles of attack up to 90 degrees (National Aeronautics and Space Administration, 1961), also by John E. Grimaud (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation at high subsonic speeds to determine stability and control characteristics of antitank missiles with ram-pressure jet controls on a ring tail (National Aeronautics and Space Administration, 1963), also by Raymond D. Vogler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation at mach numbers from 0.40 to 1.20 of the static aerodynamic and control characteristics of a model of a nonlifting reeintry capsule in combination with a rocket booster (National Aeronautics and Space Administration, 1960), also by Albin O. Pearson (page images at HathiTrust; US access only)
• Langley Research Center: Wind-tunnel investigation at Mach numbers from 0.60 to 1.20 of the static aerodynamic characteristics of a model of a possible nonlifting reentry capsule in combination with a rocket booster (National Aeronautics and Space Administration, 1960), also by Albin O. Pearson (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation at Mach numbers from 1.60 to 2.86 of the static aerodynamic characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot (National Aeronautics and Space Administration, 1962), also by David S. Shaw and William P. Henderson (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation at Mach numbers from 3.0 to 6.8 of the static aerodynamic characteristics of modified Mercury exit and escape capsule configurations (National Aeronautics and Space Administration, 1960), also by Albin O. Pearson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of a four-engine externally blowing jet-flap STOL airplane model. (National Aeronautics and Space Administration; [for sale by the National Technical Information Service, Springfield, Va.], 1970), also by Raymond D. Vogler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of a full-scale canard-configured general aviation airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Long P. Yip (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural laminar flow wing (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by Daniel G. Murri and Frank L. Jordan (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of a large-scale semispan model with an unswept wing and an upper-surface blown jet flap (National Aeronautics and Space Administration ;, 1974), also by Charles Christian Smith, W. Latham Copeland, and Arthur E. Phelps (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of a simulated gunship helicopter engine-exhaust-windstream interaction (National Aeronautics and Space Administration ;, 1974), also by John C. Wilson and Raymond E. Mineck (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration (National Aeronautics and Space Administration ;, 1975), also by Arthur E. Phelps (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of a VTOL jet-transport model with powered lift engines in pods at wing midspan or inboard (National Aeronautics and Space Administration, 1970), also by Raymond D. Vogler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by James B. Hallissy and Pamela S. Phillips (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Thomas A. Byrdsong, Cuyler W. Brooks, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory (National Aeronautics and Space Administration ;, 1975), also by Boyd Perry and George C. Greene (page images at HathiTrust)
• Langley Research Center: Wind tunnel investigation of an all flush orifice air data system for a large subsonic aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Terry J. Larson, Paul M. Siemers, Stuart G. Flechner, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of an external-flow jet-flap transport configuration having full-span triple-slotted flaps (National Aeronautics and Space Administration :, 1971), also by Lysle P. Parlett, Langley Directorate, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of an externally blown flap STOL transport model including an investigation of wall effects (National Aeronautics and Space Administration ;, 1974), also by Garl L. Gentry (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of an STOL aircraft configuration equipped with an external-flow jet flap (National Aeronautics and Space Administration :, 1969), also by Lysle P. Parlett, James P. Shivers, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration (National Aeronautics and Space Administration ;, 1973), also by Arthur E. Phelps and Charles Christian Smith (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of effect of ratio of wing chord to propeller diameter with addition of slats on the aerodynamic characteristics of tilt-wing VTOL configurations in the transition speed range (National Aeronautics and Space Administration, 1959), also by Robert T. Taylor and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of effects of variations in Reynolds number and leading-edge treatment on the aerodynamic characteristics of an externally blown jet-flap configuration (National Aeronautics and Space Administration ;, 1973), also by Lysle P. Parlett, James L. Megrail, and Charles Christian Smith (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by E. Richard White, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Kentron International (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of helicopter-rotor wake effects on three helicopter fuselage models (National Aeronautics and Space Administration ;, 1975), also by John C. Wilson and Raymond E. Mineck (page images at HathiTrust)
• Langley Research Center: A wind-tunnel investigation of parameters affecting helicopter directional control at low speeds in ground effect (National Aeronautics and Space Administration ;, 1974), also by William T. Yeager, Wayne R. Mantay, and Warren H. Young (page images at HathiTrust)
• Langley Research Center: Wind tunnel investigation of simulated helicopter engine exhaust interacting with windstream (National Aeronautics and Space Administration ;, 1974), also by Craig S. Shaw and John C. Wilson (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of sonic-boom characteristics of two simple wing models at Mach numbers from 2.3 to 4.63 (National Aeronautics and Space Administration, 1971), also by Davis S. Miller, Odell A. Morris, Harry W. Carlson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of static longitudinal and lateral characteristics of a full-scale mockup of a light single-engine high-wing airplane (National Aeronautics and Space Administration ;, 1973), also by H. Douglas Greer (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of steady-state aerodynamics of a composite-lift VTOL aircraft model (National Aeronautics and Space Administration ;, 1969), also by Matthew M. Winston, Robert J. Huston, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of the aerodynamic characteristics of a model representative of a supersonic fighter-class airplane with an external-flow jet-augmented flap in low-speed flight (National Aeronautics and Space Administration, 1959), also by William A. Newsom (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of the carry loads and mutual interference effects of 1/40-scale models of the X-15 and B-52 apirplanes in combination. (National Aeronautics and Space Administration, 1959), also by Robert T. Taylor and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: A wind-tunnel investigation of the effect of body shape on sonic-boom pressure distributions (National Aeronautics and Space Administration, 1965), also by Harry W. Carlson, Odell A. Morris, Robert J. Mack, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of the effects of blade tip geometry on the interaction of torsional loads and performance for an articulated helicopter rotor (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by William T. Yeager, Wayne R. Mantay, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Dale R. Satran (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Dale R. Satran and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of the validity of a sonic-boom-minimization concept (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Robert J. Mack, Christine M. Darden, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: A wind-tunnel investigation of the wake near the trailing edge of a deflected externally blown flap (National Aeronautics and Space Administration ;, 1974), also by William G. Johnson and Gerald E. Kardas (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation of V/STOL transport model with six wing-mounted lift fans (National Aeronautics and Space Administration, 1970), also by William A. Newsom, Frederick L. Moore, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind tunnel investigation of vortex flows on F/A-18 configuration at subsonic through transonic speeds (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Gary E. Erickson (page images at HathiTrust)
• Langley Research Center: Wind-tunnel investigation to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack (National Aeronautics and Space Administration ;, 1974), also by Paul L. Coe and William A. Newsom (page images at HathiTrust)
• Langley Research Center: Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Robert L. Stallings, Milton Lamb, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Robert J. McGhee, William D. Beasley, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Wind-tunnel roll-damping measurements of a winged space shuttle configuration in launch attitude (National Aeronautics and Space Administration ;, 1973), also by R. W. Hess and Edwin E. Davenport (page images at HathiTrust)
• Langley Research Center: Wind tunnel simulation of full scale vortices (National Aeronautics and Space Administration ;, 1973), also by James B. Rorke, Robert C. Moffitt, and United Aircraft Corporation. Sikorsky Aircraft Division (page images at HathiTrust)
• Langley Research Center: Wind-tunnel static and free-flight investigation of high-angle-of-attack stability and control characteristics of a model of the EA-6B airplane (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Frank L. Jordan and David E. Hahne (page images at HathiTrust)
• Langley Research Center: Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration (National Aeronautics and Space Administration, 1959), also by William J. Alford, William P. Handerson, and Arvo A. Luoma (page images at HathiTrust)
• Langley Research Center: Wind-tunnel study of deflected-elevator flutter encountered on a T-Tail airplane (National Aeronautics and Space Administration, 1969), also by Maynard C. Sandford, Charles L. Ruhlin, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind-tunnel study of slot spoilers for direct lift control (National Aeronautics and Space Administration, 1972), also by Dominick Andrisani, Joseph W. Stickle, Garl L. Gentry, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Paul H. Mirick, William T. Yeager, M-Nabil H. Hamouda, and United States. Army Aerostructures Directorate (page images at HathiTrust)
• Langley Research Center: Wind-tunnel tests of a full-scale model of a light twin-engine airplane with fixed auxiliary airfoil or leading-edge slot (National Aeronautics and Space Administration ;, 1974), also by Marvin P. Fink, Lucy C. White, and James P. Shivers (page images at HathiTrust)
• Langley Research Center: Wind-tunnel tests of modified cross, hemisflo, and disk-gap-band parachutes with emphasis in the transonic range (National Aeronautics and Space Administration ;, 1974), also by James T. Foughner and William C. Alexander (page images at HathiTrust)
• Langley Research Center: Wind-tunnel tests of seven static-pressure probes at transonic speeds (National Aeronautics and Space Administration, 1961), also by Francis J. Capone and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind turbine acoustics (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Harvey H. Hubbard and Kevin P. Shepherd (page images at HathiTrust)
• Langley Research Center: Wind velocity profiles measured by the smoke-trail method at the Eastern Test Range, 1962 (National Aeronautics and Space Administration, 1966), also by James C. Manning, Robert W. Miller, Robert M. Henry, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wind velocity profiles measured by the smoke-trail method at Wallops Island, Virginia, 1959 to 1962 (National Aeronautics and Space Administration, 1965), also by Robert W. Miller, Mickey G. Rowe, Robert M. Henry, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Langley Research Center: Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Robert L. Stallings, Milton Lamb, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Langley Research Center: Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at Mach numbers from 0.8 to 1.4 (National Aeronautics and Space Administration, 1959), also by Clarence L. Gillis and A. James Vitale (page images at HathiTrust)
• Langley Research Center: X-ray spectra produced when thick silicon targets are bombarded with 1.05 and 1.25 million volts electrons (National Aeronautics and Space Administration ;, 1966), also by Jag J. Singh, Chris Gross, and Richard Adams (page images at HathiTrust)
• Langley Research Center: Zero thermal expansion composites of high strength and stiffness (National Aeronautics and Space Administration ;, 1969), also by Norris F. Dow, B. Walter Rosen, and General Electric Company (page images at HathiTrust)