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Aircraft safety and noise

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• Investigation of water-pond arresting of a dynamic model of a jet transport (National Aeronautics and Space Administration :, 1961), by William C. Thompson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Noise considerations in the design and operation of V/STOL aircraft (National Aeronautics and Space Administration :, 1961), by Domenic J. Maglieri, Harvey H. Hubbard, David A. Hilton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Survey of altitude-measuring methods for the vertical separation of aircraft (National Aeronautics and Space Administration :, 1961), by William Gracey and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Airspeed operating practices of turbine-powered commercial transport airplanes (National Aeronautics and Space Administration :, 1962), by Thomas L. Coleman, Walter G. Walker, Martin R. Copp, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of parachutes at mach numbers from 1.6 to 3 (National Aeronautics and Space Administration :, 1961), by Julian D. Maynard and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Skid landings of airplanes on rocker-type fuselages. (National Aeronautics and Space Administration :, 1961), by Wilbur L. Mayo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of multiple-nozzle geometry on jet noise generation. (National Aeronautics and Space Administration :, 1961), by Vern G. Rollin 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 (National Aeronautics and Space Administration :, 1961), by Russell L. Schott 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 (National Aeronautics and Space Administration :, 1961), by David H. Hickey, Kiyoshi Aoyagi, William H. Tolhurst, 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 (National Aeronautics and Space Administration :, 1962), by L. Stewart Rolls, Fred J. Drinkwater, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental and calculated flow fields produced by airplanes flying at supersonic speeds (National Aeronautics and Space Administration :, 1960), by Harriet J. Smith 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 (National Aeronautics and Space Administration :, 1962), by Odell A. Morris 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. (National Aeronautics and Space Administration :, 1962), by Walter B. Horne, Trafford J.W. Leland, 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 (National Aeronautics and Space Administration :, 1961), by Joseph W. Stickle and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Repeatability, drift, and after effect of three types of aircraft altimeters (National Aeronautics and Space Administration :, 1961), by William Gracey, Richard E. Stell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of a balloon as a towed deceleration at mach numbers from 1.47 to 2.50 (National Aeronautics and Space Administration :, 1961), by John T. McShera, J. Wayne Keyes, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation of landing-contact conditions for a large turbojet transport during routine daylight operations (National Aeronautics and Space Administration :, 1960), by Joseph W. Stickle, Norman S. Silsby, 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 (National Aeronautics and Space Administration :, 1961), by Willard D. Coles, William H. Swann, John A Mihaloew, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Ground measurements of the shock-wave noise from supersonic bomber airplanes in the altitude range from 30,000 to 50,000 feet. (National Aeronautics and Space Administration :, 1961), by Domenic J. Maglieri, Harvey H. Hubbard, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• In-flight noise measurements for three Project Mercury vehicles (National Aeronautics and Space Administration :, 1962), by William H. Mayes, Charles A. Hardesty, David A. Hilton, 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 (National Aeronautics and Space Administration :, 1961), by Paul A. Hunter, William L. Alford, Christopher C. Kraft, 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. (National Aeronautics and Space Administration :, 1961), by William Gracey, Jo Ann Shipp, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic performance characteristics of several jet noise suppressors (National Aeronautics and Space Administration :, 1960), by James W. Schmeer, Marlowe D. Cassetti, Leland B. Salters, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A flight study of a power-off landing technique applicable to re-entry vehicles. (National Aeronautics and Space Administration :, 1960), by Richard S. Bray, Maurice D. White, Fred J. Drinkwater, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight-determined aerodynamic-noise environment of an airplane nose cone up to a Mach number of 2 (National Aeronautics and Space Administration :, 1962), by Norman J. McLeod and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Studies in far-field acoustic propagation. Richard N. Tedrick, Roy Peterson, T. Kleffman, Wade D. Dorland, R. Ewing, and D. Church. (National Aeronautics and Space Administration :, 1961), by Richard N. Tedrick, D. Church, R. Ewing, Wade D. Dorland, T. Kleffman, Roy Peterson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Far-field noise characteristics of Saturn static tests (National Aeronautics and Space Administration :, 1961), by Wade D. Dorland and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A brief evaluation of helisopter wake as a potential operational hazard to aircraft (National Aeronautics and Space Administration :, 1962), by Andrew B. Connor, Thomas C. O'Bryan, 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 (National Aeronautics and Space Administration :, 1961), by Russell D. Shattuck and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A preliminary study of the acoustic transmission loss of two fiberglas nose cone shapes (National Aeronautics and Space Administration :, 1961), by Vern G. Rollin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation of the influence of lift on sonic-boom intensity by means of wind-tunnel measurements of the pressure fields of several wing-body combinations at a mach number of 2.01 (National Aeronautics and Space Administration :, 1961), by Harry W. Carlson 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 (National Aeronautics and Space Administration :, 1960), by Andrew B. Connor and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Operational experiences of turbine-powered commercial transport airplanes (National Aeronautics and Space Administration :, 1962), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• VTOL height-control requirements in hovering as determined from motion simulation study (National Aeronautics and Space Administration :, 1962), by John F. Garren, Arthur Assadourian, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of VTOL approach methods by use of ground-controlled-approach procedures (National Aeronautics and Space Administration :, 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 (National Aeronautics and Space Administration :, 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 (National Aeronautics and Space Administration :, 1962), by Harry W. Carlson 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 (National Aeronautics and Space Administration :, 1961), by William A. McGowan and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Electric spark ignition in carbon-vane fuel pumps (National Aeronautics and Space Administration :, 1961), by John A. Campbell, Robert G. Dorsch, Richard J. Parker, and United States National Aeronautics and Space Administration (page images at HathiTrust)

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