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Aircraft design

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• Potential structural materials and design concepts for light aircraft (National Aeronautics and Space Administration ;, 1969), by Ladislao Pazmany, Inc San Diego Aircraft Engineering, NASA Headquarters Mission Analysis Division, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Design and experimental results of a highly loaded, low solidity tandem rotor (National Aeronautics and Space Administration ;, 1971), by James L. Bettner, Langley Research Center, and General Motors Corporation (page images at HathiTrust)
• Conceptual design study of 1985 commercial tilt rotor transports. Volume 1, VTOL design summary (National Aeronautics and Space Administration ;, 1975), by J. A. DeTore, K. W. Sambell, and Bell Helicopter Company (page images at HathiTrust)
• A study of NACA and NASA published information of pertinence in the design of light aircraft. Volume II, Aerodynamics and aerodynamic loads (National Aeronautics and Space Administration ;, 1970), by James C. Williams, John N. Perkins, Delbert C. Summey, Langley Research Center, and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• A study of NACA and NASA published information of pertinence in the design of light aircraft. Volume III, Propulsion subsystems, performance, stability and control, propellers, and flight safety (National Aeronautics and Space Administration ;, 1970), by Clifford J. Moore, Dennis M. Phillips, Langley Research Center, and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• Effectiveness of an all-movable horizontal tail on an unswept-wing and body combination for Mach numbers from 0.60 to 1.40 (National Aeronautics and Space Administration, 1959), by Louis S. Stivers and Ames Research Center (page images at HathiTrust)
• 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), by Henry A. Lee, Charles E. Libbey, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Low-speed wind-tunnel investigation of a wingless jet VTOL transport model (National Aeronautics and Space Administration, 1959), by Marion O. McKinney and Langley Research Center (page images at HathiTrust)
• Flight investigation of an automatic pitchup control (National Aeronautics and Space Administration, 1960), by George J. Hurt, James B. Whitten, and Langley Research Center (page images at HathiTrust)
• An analysis of incremental horizontal-tail loads measured on a swept-wing bomber airplane in sideslip maneuvers (National Aeronautics and Space Administration, 1959), by William A. McGowan and Langley Research Center (page images at HathiTrust)
• Investigation of double slotted flaps on a swept-wing transport model (National Aeronautics and Space Administration, 1959), by Rodger L. Naeseth, Edwin E. Davenport, and Langley Research Center (page images at HathiTrust)
• Full-scale wind-tunnel investigation of the longitudinal characteristics of a tilting-rotor convertiplane (National Aeronautics and Space Administration, 1959), by David G. Koenig, Mark W. Kelly, Richard K. Greif, and Ames Research Center (page images at HathiTrust)
• Design criteria for the future of flight controls : proceedings of the Flight Dynamics Laboratory Flying Qualities and Flight Control Symposium, 2-5 March, 1982. (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), by Flight Dynamics Laboratory Flying Qualities and Flight Control Symposium (1982 : Dayton), D. W. Potts, S. G. Fuller, Air Force Flight Dynamics Laboratory (U.S.), and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)

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