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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 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 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 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: 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 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)
• 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: 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; US access only)
• 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 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: 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 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)
• 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 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 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: 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: 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: 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: 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: 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; US access only)
• 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; US access only)
• 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 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 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)
• 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: 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 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 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 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 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)
• 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: 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: 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, 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 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 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 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 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; US access only)
• 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: 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; US access only)
• 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 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)
• 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 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 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 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 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; US access only)
• 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: 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)
• 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)
• 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: 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 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 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: 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 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)
• 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 study of vertical impacts of an LM-type landing gear assembly under simulated lunar gravity (lunar module). (1968), also by United States National Aeronautics and Space Administration, John Locke McCarty, and Huey D. Carden (page images at HathiTrust; US access only)
• 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; US access only)
• 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: 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; US access only)
• 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: 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: 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; US access only)
• 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 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: 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)
• 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: 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: An hovering investigation of an extremely flexible lifting rotor (National Aeronautics and Space Administration, 1968), also by Matthew M. Winston and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• 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: 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: 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; US access only)
• 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 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; US access only)
• 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 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: 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: Investigation of a class of bodies that generate far-field sonic-boom shock strength and impulse independent of body length and volume (National Aeronautics and Space Administration, 1969), also by Raymond L. Barger, Frank L. Jordan, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• 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 compartmented-gas-bag landing system having multiple-impact capabilities. (1968), also by United States National Aeronautics and Space Administration and John R. McGehee (page images at HathiTrust; US access only)
• 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 Administra