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Aircraft

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• In-flight use of traversing boundary-layer probes / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Edwin J. Saltzman, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Charles F. Whitcomb, Chris C. Critzos, Philippa F. Brown, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A flight evaluation of a VTOL jet transport under visual and simulated instrument conditions (Washington, DC : National Aeronautics and Space Administration, 1972), by Curt A. Holzhauser, James M. Patton, Robert C. Innis, Samuel A. Morello, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some loading conditions imposed by ground turning maneuvers with three jet transport airplanes (Washington : NASA ; Springfield, Va. : avail. from National Technical Information Service, 1972), by Albert W. Hall, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Prediction of aircraft condensation trails project contrails. (Ft. Belvoir : Defense Technical Information Center, 31 Oct 1961), by James E. Jiusto and Cornell Aeronautical Lab Inc Buffalo NY. (page images at HathiTrust; US access only)
• Report to the Congress on energy conservation potential of off-highway recreational motor vehicles. ([Washington, D.C.?] : U.S. Department of Transportation, 1979), by United States. Department of Transportation (page images at HathiTrust)
• Development of a safety and planning program /, by Richard C. Gazley, United States. Civil Aeronautics Authority, and United States. Bureau of Air Commerce (page images at HathiTrust)
• Hazards of lightning discharge to aircraft /, by G. A. Faucher, H. O. Curtis, and Air Force Cambridge Research Center (U.S.). Geophysics Research Directorate (page images at HathiTrust)
• Solving titanium fabrication and reliability problems in aircraft production /, by W. Stuart Lyman, A. M. Federico, C. T. Olofson, and issuing body Defense Metals Information Center (U.S.) (page images at HathiTrust)
• Preliminary design information on recrystallized Mo-0.5Ti alloy for aircraft and missiles /, by W. P. Achbach, R. J. Favor, and issuing body Defense Metals Information Center (U.S.) (page images at HathiTrust)
• Designations of alloys for aircraft and missiles /, by R. M. Evans and issuing body Defense Metals Information Center (U.S.) (page images at HathiTrust)
• Helicopters in emergency medical service : NHTSA experience to date, December 1972 (Washington : U.S. Govt.Print.Off, [1973]), by United States. National Highway Traffic Safety Administration (page images at HathiTrust)
• Aviation engineers. (Washington, U.S. Govt. Print. Off., 1944), by United States War Department (page images at HathiTrust)
• Transonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading edge sweep / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Paul G. Fournier, B. Ann Bell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static aerodynamic characteristics of a Scout fin with an enlarged tip control at Mach numbers from 0.40 to 4.63 / (Washington, D.C.: National Aeronautics and Space Administration:, 1971), by Robert J. Keynton (page images at HathiTrust; US access only)
• Air service medical manual ... (Washington, Government printing office, 1918), by United States. Office of the Chief of Air Corps (War Department) (page images at HathiTrust)
• NATS manual / (Washington, D.C. : Naval Air Transport Service, 1944), by Naval Air Transport Service (page images at HathiTrust)
• Internal-performance evaluation of a two-position divergent shroud ejectro / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by James R. Mihaloew, Andrew J. Stofan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• New methods and results for quantification of lightning-aircraft electrodynamics / (Washington, D.C. : National Aeronautics and Space Administration, 1987), by Felix L. Pitts and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of water-pond arresting of a dynamic model of a jet transport / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by William C. Thompson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Considerations of methods of improving helicopter efficiency / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Richard C. Dingeldein and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Noise considerations in the design and operation of V/STOL aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Domenic J. Maglieri, Harvey H. Hubbard, David A. Hilton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some recent studies in structural dynamics of rotor aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by George W. Brooks, Milton A. Silveira, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Survey of altitude-measuring methods for the vertical separation of aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by William Gracey and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by James P. Shivers and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Airspeed operating practices of turbine-powered commercial transport airplanes / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Thomas L. Coleman, Walter G. Walker, Martin R. Copp, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight controllability limits and related human transfer functions as determined from simulator and flight tests / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Lawrence W. Taylor, Richard E. Day, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effect of thrust minus base drag of exchanging base area for nozzle expansion in supersonic nozzles at transonic mach numbers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Travis H. Slocumb, Earl H. Andrews, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight investigation of effects of selected operatings conditions on the bending and torsional moments encountered by a helicopter rotor blade / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by LeRoy H. Ludi and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Skid landings of airplanes on rocker-type fuselages. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Wilbur L. Mayo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Jack F. Runckel and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of ratio of jet area to total area and of pressure on lift augmentation of annular jets in ground effect under static conditions / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1961]), by Kenneth W. Goodson, James H. Otis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Launch characteristics of the X-15 research airplane as determined in flight / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Gene J. Matranga and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Structural-loads surveys on two tilt-wing VTOL configurations / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by John F. Ward and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight investigation of some effects of a vane-controlled gust-alleviation system on the wing and tail loads fo a transport airplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Russell L. Schott and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A flight determination of the attitude control power and damping requirements for a visual hovering task in variable stability and control X-14A research vehicle / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by L. Stewart Rolls, Fred J. Drinkwater, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigating of the drag and static stability characteristics of four helicopter fuselage models / George E. Sweet and Julian L. Jenkins Jr. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by George E. Sweet, Julian L. Jenkins, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A Wind-tunnel investigation of the longitudinal aerodynamic charachteristics of two full-scale helicopter fuselage models with appendages / Julian L. Jenkins, Matthew M. Winston and George E. Sweet. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Julian L. Jenkins, George E. Sweet, Matthew M. Winston, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Longitudinal stability and control of a tilt-wing VTOL aircraft model with rigid and flapping propeller blades / Louis P. Tosti. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Louis P. Tosti and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Kalman J. Grunwald, Kenneth W. Goodson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Roxanah B. Yancey and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measured surface defects on typical transonic airplanes and analysis of their drag contribution / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Elmer A. Horton, Neal Tetervin, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul G. Fournier and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed aerodynamic characteristics of a model of a hypersonic research airplane at angles of attack up to 90 degrees for a range of Reynolds numbers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by James S. Bowman, William D. Grantham, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hovering and transition flight tests of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Charles C. Smith and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measurements of the time-averaged and instantaneous induced velocities in the wake of a helicopter rotor hovering at high tip speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Harry H. Heyson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Equations for the induced velocities near a lifitng rotor with nonuniform azimuthwise vorticity distribution / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Harry H. Heyson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of X-15 landing approach and flare characteristics determined from the first 30 flights / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Gene J. Matranga and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Large-scale wind-tunnel tests of an airplane model with an unswept, tilt wing of aspect ration 5.5, and with four propellers and blowing flaps / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by James A. Weiberg, Curt A. Holzhauser, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed wind-tunnel investigation of a reflection plane wing equipped with partial-span jet-augmented flaps / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by James H. Otis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic aerodynamic characteristics of a wing-body combination having a 52.2⁰ sweptback wing of aspect ratio 3 with conical camber and designed for a mach number of 2/ (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by William B. Igoe, Maarlowe D. Cassetti, Richard J. Re, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Random deviations from cruise altitudes of a turbojet transport transport at altitudes between 20,000 and 41,000 feet. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by William Gracey, Jo Ann Shipp, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical calculations of the pressures, forces and moments due to various larteral motions acting on tapered sweptback vertical tails with superesonic leading and trainling edges / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Kenneth Margolis, Miriam H. Elliott, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static stability and control of canard configurations at mach numbers from 0.70 to 2.22 - trangular wing and canard with twin vertical tails / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Victor L. Peterson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A flight study of the conversion maneuver of a tilt-wing VTOL aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1959]), by Lovic P. Thomas and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Large-scale wind-tunnel tests of a wingless vertical take-off and landing aircraft - preliminary results. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by David G. Koenig, James A. Brady, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental and theoretical study of a rectangular wing in a vortical wake at low speed / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Willard G. Smith, Frank A. Lazzeroni, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A flight study of the conversion maneuver of a tilt-duct VTOL aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Robert J. Tapscott, Henry L. Kelley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of a pilot-airplane lateral instability experienced with the X-15 airplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Lawrence W. Taylor and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical evaluation of hypersonic forces moments and stability derivatives for combinations of flat plates, including effects of blunt leading edges, by Newtonian impact theory / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Walter B. Olstad and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic performance characteristics of several jet noise suppressors / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by James W. Schmeer, Marlowe D. Cassetti, Leland B. Salters, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of a 1/4-inch scale model a tilt-wing VTOL aircraft at high angles of wing incidence / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Louis P. Tosti and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental investigation of boundary-layer control for drag reduction of a swept-wing section at low speed and high reynolds numbers. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Donald E. Gault and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Full scale wind-tunnel tests of blowing boundary-layer control applied to a helicopter rotor / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by John L. McCloud, James A. Brady, Leo P. Hall, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The design of feedback control systems containing a saturation type nonlinearity. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Stanley F. Schmidt, Eleanor V. Harper, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical flutter analysis of flat rectangular panels in uniform coplanar flow with arbitrary direction / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Eldon E. Kordes, Richard B. Noll, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• X-15 airplane stability augmentation system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Lawrence W. Taylor, George B. Merrick, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mission planning and operational procedures for the X-15 airplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert G. Hoey, Richard E. Day, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effect of lateral directional control coupling on pilot control of an airplane as determined in flight and in a fixed base flight simulator / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Richard F. Vomaske, Fred J. Drinkwater, Melvin Sadoff, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some examples of the applications of the transonic and supersonic area rules to the prediction of wave drag. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert L. Nelson, Clement J. Welsh, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lateral stability and control characteristics of a four-propleer deflected-slipstream VTOL model inculding the effects of ground proximity / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Richard E. Kuhn, Kalman J. Grunwald, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A preliminary piloted simulator and flight study of height control requirements for VTOL aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Ronald M. Gerdes and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed wind-tunnel investigation to determine the flight characteristics of a model of a parawing utility vehicle. Joseph L. Johnson. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Joseph L. Johnson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Subsonic wind-tunnel investigation of errors indicated by total-pressure tubes in the flow field of a body simulating the nose of the X-15 research airplane. William J. Alford Jr. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William J. Alford and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A rigidly forced oscillation system for meaasuring dynamic-stability parameters in transonic and supersonic wind tunnels / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Albert L. Braslow, Cullen Q. Lee, Harleth G. Wiley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight-test investigation of a model of an aerial vehicle supported by four unshrouded propellers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Robert H. Kirby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of forebody length on the stability and control characteristics at a Mach number of 2.01 of a canard airplane configuration with a trapezoidal aspect-ratio-3 wing / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by M. Leroy Spearman, Cornelius Driver, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Pressure distributions at Mach number 2.05 on a series of highly swept arrow wings employing various degrees of twist and camber / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Harry W. Carlson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics in pitch of several ring-wing-body configurations at a mach number of 2.2. Odell Morris. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Odell A. Morris and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A tabulation of section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for four swept wings having the same planform but different surface shapes. Emma Jean Landrum. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Emma Jean Landrum and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Force-test investigation of a model of an aerial vehicle supported by four unshrouded propellers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Robert H. Kirby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental study of the effect of downwash from a twin-propeller VTOL aircraft on several types of ground surfaces / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Thomas C. O'Bryan and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Review of the X-15 program Joseph Weil. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Joseph Weil and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A Simple solar orientation control system for space vehicles. Seymour Salmirs, S. Lawrence Kessler and Otis J. Parker. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Seymour Salmirs, Otis J. Parker, S. Lawrence Kessler, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Advanced static inverter utilizing digital techniques and harmonic cancellation / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Dorrance L. Anderson, Carl E. Winkler, Albert E. Willis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed aerodynamic charachteristics of a cargo airplane configuration having split flaps located ahead of the wing trailing edge and leading- and trailing-edge flaps on the Canard Control. Bernard Spencer Jr. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Bernard Spencer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Sound pressures and correlations of noise on the fuselage of a jet aircraft in flight / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Russell D. Shattuck and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A summary of operating conditions experienced by three military helicopters and a mountain-based commercial helicopter / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Andrew B. Connor and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed measurements of static and oscillatory lateral stability derivatives of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1960]), by Robert E. Shanks, Charles C. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed investigation of a full-span internal-flow jet-augmented flap on a high-wing model with a 35 degree swept wing of aspect ratio 7.0 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Thomas R. Turner and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of a large-scale unswept wing-body-tail configuration with blowing applied over the flap and wing leading edge / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Huel Clyde McLemore, John B. Peterson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A Wind-tunnel investigation of pressure fluctuations on the upper vertical tail of the X-15 when mated to the B-52 carrier airplane / John W. McKee and Thomas A. Byrdsong. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by John W. McKee, Thomas A. Byrdsong, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight calibrations of fuselage static-pressure-vent installations for three types of transports / Norman S. Silsby and Joseph W. Stickle. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Norman S. Silsby, Joseph W. Stickle, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of water-absorbent materials as possible heat sinks for hypersonic and reentry vehicles Robert P. Dengler and Reeves P. Cochran. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert P. Dengler, Reeves P. Cochran, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measurements of the response of two light airplanes to sonic booms / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1963]), by Domenic J. Maglieri, Garland J. Morris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Internal-performance evaluation of two fixed-divergent-shroud ejectors / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by James R. Mihaloew and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of multiple-nozzle geometry on jet noise generation. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Vern G. Rollin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the longitudinal characteristics of a large-scale jet tranport model equipped with controllable thrust reversers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by David H. Hickey, Kiyoshi Aoyagi, William H. Tolhurst, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamics of a fan-in-fuselage model / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Ralph L. Maki, David H. Hickey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta wing and an unswept horizontal tail. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Alan B. Kehlet and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Longitudinal trim characteristics of a deflected slipstream V/Stol aircraft during level flight at transition flight speeds / Howard L. Turner and Fred J. Drinkwater III. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Howard L. Turner, Fred J. Drinkwater, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Slipstream flow around several tilt-wing VTOL aircraft models operating near the ground / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William A. Newsom, Louis P. Tosti, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A wind-tunnel investigation at a Mach number of 2.01 of the sonic-boom characteristics of three wing-body combinations differing in wing longitudinal location / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Odell A. Morris and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight investigation of the longitudinal stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William A. Newsom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Pressure distributions on two-dimensional sharp-leading-edge flat plates with sweep angles of 0 degrees, 30 degrees, and 45 degrees at a mach number of 6 and angles of attack from 0 degrees to 90 degrees / James G. Hondros. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by James G. Hondros and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight-tested investigation of ailerons as a source of yaw control on the VZ-2 tilt-wing aircraft / Robert J. Pegg (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert J. Pegg and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Influence of the tire tread pattern and runway surface condition on breaking friction and rolling resistance of a modern aircraft tire / Walter B. Horne and Trafford J.W. Leland. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Walter B. Horne, Trafford J.W. Leland, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Application of monte carlo technique for determining maneuvering loads from statistical information on airplane motions / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Harold A. Hamer, Wilber B. Huston, John P. Mayer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William I. Scallion and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of a four-propeller tilt-wing VTOL model with twin vertical tails, including effects of ground proximity / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Kalman J. Grunwald and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Edward C. Polhamus, Kenneth P. Spreemann, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stability and control characteristics of a model of an aerial vehicle supported by four ducted fans / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Lysle P. Parlett and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Force-test investigation of the stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William A. Newsom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation of landing-contact conditions for two large turbojet transports and a turboprop transport during routine daylight operations / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Joseph W. Stickle and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45 degree sweptback wing at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Donald D. Arabian, Charles F. Reid, Jack F. Runckel, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of low-aspect-ratio wings in close proximity to the ground/ (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Marvin P. Fink, James L. Lastinger, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Free-flight investigation of radio-controlled models with parawings / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Donald E. Hewes and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of interference of a deflected jet with free stream and ground on aerodynamic characteristics of a semispan Delta-wing VTOL model / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Kenneth P. Spreemann and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stability and control characteristics of a small-scale model of an ariel vehicle supported by two ducted fans / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Lysle P. Parlett and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of body-mounted lateral controls and speed brakes on the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.98 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by F. E. West and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A transonic investigation of changing indentation design Mach number on the aerodynamic characteristics of a 45 degree sweptback-wing-body combination designed for high performance / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Donald L. Loving and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel tests of two full-scale helicopter fuselages (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by James C. Biggers and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic and hydrodynamic characteristics of a model of a 500,000-pound high-subsonic multijet logistics transport seaplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1961]), by Walter J. Kapryan, Irving Weinstein, Kenneth W. Goodson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Ground and in-flight acoustic and performance characteristics of jet-aircraft exhaust noise supressors / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Willard D. Coles, William H. Swann, John A Mihaloew, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed investigation of the effects of frequency and amplitude of oscillation in sideslip on the lateral stability derivatives of a 60 degree delta wing, a 40 degree sweptback wing and an unswept wing / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Jacob H. Lichtenstein, James L. Williams, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Repeatability of the over-all errors of an airplane altimeter installation in landing-approach operations / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by William Gracey, Joseph W. Stickle, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the flow in a rectangular cavity in a flat plate at a mach number of 3.55 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Russell W. McDearmon and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A flight investigation of an automatic gust-alleviation system in a transport airplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul A. Hunter, William L. Alford, Christopher C. Kraft, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A note on the drag due to lift of delta wings at mach numbers up to 2.0 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert S. Osborne, Thomas C. Kelly, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Handling qualities of the XB-70 airplane in the landing approach. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1970]), by Donald T. Berry, Bruce G. Powers, Flight Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Proposed technique for launching instrumented balloons into tornadoes. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1971]), by Frederick C. Grant, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A reaction attitude control system for jet VTOL research aircraft. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1970]), by Frank A. Pauli, James R. Rogers, Tom G. Sharpe, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Digital automatic data reduction techniques used in a 1000-flight biomedical study / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1971), by Richard Carpenter, James Roman, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fan and wing force data from wind-tunnel investgation of a 0.38-meter (15-IN.) diameter VTOL model lift fan installed in a two-dimensional wing / (Washington, DC : National Aeronautics and Space Administration, 1972), by Joseph A. Yuska, James H. Diedrich, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of an automatic spin-prevention system for fighter airplanes / (Washington, DC : National Aeronautics and Space Administration, 1972), by William P. Gilbert, Charles E. Libbey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Operational technique for transition of several types of V/STOL aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Fred J. Drinkwater and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of a large-scale model with a high disk-loading lifting fan mounted in the fuselage / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Kiyoshi Aoyagi, Richard A. deSavigny, David H. Hickey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Norman M. McFadden, Donovan R. Heinle, Richard F. Vomaske, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Characteristics at mach number of 2.03 of a series of wings having various spanwise distributions of thickness ration and chord / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by A. Warner Robins, Charlie M. Jackson, Roy V. Harris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An analysis of the flapwise bending frequencies and mode shapes of rotor blades having two flapping hinges to reduce vibration levels / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by George W. Brooks, H. Wayne Leonard, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A wind-tunnel investigation of a 4-foot-diameter ducted fan mounted on the tip of a semispan wing / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul F. Yaggy, Kenneth W. Mort, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Attitude control requirements for hovering determined through the use of a piloted flight simulator / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Alan E. Faye and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by William C. Sleeman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hovering flight investigation of two methods of controlling a man-carrying ducted-fan vehicle of the flying-platform type. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Lysle P. Parlett and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Normal-force and hinge-moment characteristics at transonic speeds of flap-type ailerons at three spanwise locations on a 4-percent-thick sweptback-wing-body model and pressure-distribution measurements on an inboard aileron. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Jack F. Runckel, Gerald Hieser, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of an axisymmetric internal compression inlet at a mach number of about 3.8 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by John H. Lundell, Lewis A. Anderson, Richard Scherrer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic and supersonic wind-tunnel tests of wing-body combinations designed for high efficiency at a mach number of 1.41 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Frederick C. Grant, John R. Sevier, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Operational experiences of turbine-powered commercial transport airplanes / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for two trapezoidal and three delta wings having different surface shapes / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Emma Jean Landrum and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation to determine the discharge and thrust characteristics of auxiliary-air outlets for a stream Mach number of 3.25 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Allen R. Vick and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed longitudinal characteristics of a airplane configuration including effects of canard and wing trailing-edge flap controls in combination / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Bernard Spencer, William C. Sleeman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of afterbody ejection configurations on the performance at transonic speeds of a pylon-supported Nacelle model having a hot-jet exhaust / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by John M. Swihart, Harry T. Norton, Charles E. Mercer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by James H. Otis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of VTOL approach methods by use of ground-controlled-approach procedures / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by James P. Trant, Joseph S. Algranti, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation of landing-contact conditions for several turbojet transports during routine daylight operations at New York International Airport / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Joseph W. Stickle and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The lower bound of attainable sonic-boom overpressure and design methods of approaching this limit / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Harry W. Carlson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Charles F. Whitcomb, Harry T. Norton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Calculated normal load factors on light airplanes traversing the trailing vortices of heavy transport airplanes / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by William A. McGowan and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measurement of the maximum altitude attained by the X-15 airplane powered with interim rocket engines / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Wendell H. Stillwell, Terry J. Larson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An exploratory study of a parawing as a high-lift device for aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Rodger L. Naeseth and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aircraft noise and sonic boom; selected references. (Washington, 1969), by United States. Dept. of Transportation. Library Services Division and Maria R. Haywood (page images at HathiTrust; US access only)
• A narrative of the two aerial voyages of Doctor Jeffries with Mons. Blanchard; with meteorological observations and remarks. The first voyage, on the thirtieth of November, 1784 from London into Kent: the second, on the seventh of January, 1785, from England into France. ([New York, 1941]), by John Jeffries, Institute of the Aerospace Sciences. Aeronautical archives, and N.Y.) United States. Work Projects Administration (New York (page images at HathiTrust)
• Analysis of lateral-directional stability characteristics of a twin-jet fighter airplane at high angles of attack / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Joseph R. Chambers, Ernie L. Anglin, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Emergency care systems demonstration projects. Volume 2: the emergency care system. Final report. (1968), by Kenneth R. Bordner, C. Burkhart, John M. Howard, and Albert G. D. Levy (page images at HathiTrust)
• Police traffic services handbook for governor's highway safety representatives. Final report. (1973), by A. G. Johnson, Norman Darwick, R. Sostkowski, F. Roberson, A. Smith, and B. Pedersen (page images at HathiTrust)
• Analysis and design of freeway incident response systems. (1974), by Chyi Kang Lu and Adolph D. May (page images at HathiTrust)
• Ride quality symposium. 1975. Technical memorandum. (1975), by 11-12 Aug 1975 Ride Quality Symposium (page images at HathiTrust)
• Interagency symposium on university research in transportation noise. Third. (1975), by 3rd Interagency Symposium on University Research in Transportation Noise (page images at HathiTrust)
• Development of a systems risk methodology for single and multi-modal transportation systems. Final report. (1979), by Alfredo Hua-Sing Ang and J. Briscoe (page images at HathiTrust)
• Performance evaluation of child restraint systems. Final report. (1982), by K. N. Naab (page images at HathiTrust)
• The role of aircraft panel materials in cabin fires and their properties. Final report. (1985), by James G. Quintiere, Vytenis Babrauskas, L. Cooper, M. F. Harkleroad, K. Steckler, and A. Tewarson (page images at HathiTrust)
• Summary report - full-scale transport controlled impact demonstration program. Final report. (1987) (page images at HathiTrust)
• Accident/incident data analysis database summaries. Volume I. (1989), by T. P. Murphy and R. J. Levendoski (page images at HathiTrust)
• Reliability and performance of friction measuring tires and friction equipment correlation. Final report. (1990), by T. H. Morrow (page images at HathiTrust)
• An assessment of the potential for neck injury due to padding of aircraft interior walls for head impact protection. Final report. (1993), by R. Armenia-Cope, J. H. Marcus, R. V. Gowdy, and Rick DeWeese (page images at HathiTrust)
• Full-scale fire testing of seat component materials. (1993), by Patricia Cahill (page images at HathiTrust)
• The development of a horizontal impact sled facility and subsequent crashworthiness experiments. Final report. (1993), by Walter Bernhart, Joseph A. Mitchell, Karl W. Petzold, and Juan C. Rodriguez (page images at HathiTrust)
• A comparable systems analysis: comparing automated highway systems to air traffic management. Final report. (1994), by M. J. Hoffman and W. H. Corwin (page images at HathiTrust)
• The effect of instrument approach procedure chart design on pilot search speed and response accuracy: flight test results. Final report. (1995), by D. W. Osborne, M. Stephen Huntley, J. W. Turner, and C. M. Donovan (page images at HathiTrust)
• Transportation technology plan. (1998) (page images at HathiTrust)
• Evaluation of a head injury criteria component test device. (Washington, D.C. : Office of Aerospace Medicine, Federal Aviation Administration ; [Springfield, Va. : Available through the National Technical Information Service, 2004), by Rick DeWeese and D. M. Moorcroft (page images at HathiTrust)
• Toxicological profile for jet fuels JP-4 and JP-7 / ([Atlanta, Ga.] : U. S. Department of Health and Human Services, Public Health Service, Agency for Toxic Substances and Disease Registry, 1995), by Research Triangle Institute, United States. Agency for Toxic Substances and Disease Registry, and Clement International Corporation (page images at HathiTrust)
• Toxicological profile for JP-5 and JP-8 / ([Atlanta Ga.] : U.S. Dept. of Health and Human Services, Public Health Service, Agency for Toxic Substances and Disease Registry, 1998), by Research Triangle Institute and United States. Agency for Toxic Substances and Disease Registry (page images at HathiTrust)
• Airliner cabin air quality : hearing before the Subcommittee on Aviation of the Committee on Public Works and Transportation, House of Representatives, One Hundred Third Congress, second session, May 18, 1994. (Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 1994), by United States. Congress. House. Committee on Public Works and Transportation. Subcommittee on Aviation (page images at HathiTrust)
• International conference on mobility and transport of elderly and handicapped persons. Third. Proceedings. Final report. (1984), by William G. Bell, Norman Ashford, and 3rd International Conference on Mobility and Transport of Elderly and Handicapped Persons (page images at HathiTrust)
• Air ambulance guidelines. (1986) (page images at HathiTrust)
• The Pilot-Vehicle Interface. Final report. (1993), by L. Harrison, J. Janowitz, and M. Castronuovo (page images at HathiTrust)

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