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Supersonic transports

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• NASA research on materials applicable to supersonic transports / (Washington, D.C. : National Aeronautics and Space Administration ; Washington, D.C. : For sale by the Office of Technical Services, Department of Commerce [distributor], 1964), by Herbert F. Hardrath, George J. Heimerl, and Langley Research Center (page images at HathiTrust)
• Longitudinal aerodynamic characteristics at Mach numbers from 0.50 to 1.19 of a supersonic transport model with a modified M wing / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1967), by Edward J. Ray, Robert T. Taylor, and Langley Research Center (page images at HathiTrust)
• High-lift characteristics of a variable-sweep supersonic transport model with a blended engine-fuselage and engine-mounted horizontal tails / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by Vernard E. Lockwood and Langley Research Center (page images at HathiTrust)
• Lateral directional stability characteristics at mach 2.3 to 3.5 of a supersonic transport model with various outboard vertical-tail locations / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1965), by William A. Corlett and Langley Research Center (page images at HathiTrust)
• A simulator study of the effectiveness of a pilot's indicator which combined angle of attack and rate of change of total pressure as applied to the take-off rotation and climbout of a supersonic transport / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Albert W. Hall, Jack E. Harris, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Take-off distances of a supersonic transport configuration as affected by airplane rotation during the take-off run / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Albert W. Hall, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Salt-stress-corrosion cracking of residually stressed Ti-8Al-1Mo-1V brake-formed sheet at 550° F (561° K) / (Washington, D.C. : National Aeronautics and Space Administration ; Washington, D.C. : For sale by the Office of Technical Services, Department of Commerce [distributor], 1965), by Richard A. Pride, John M. Woodard, and Langley Research Center (page images at HathiTrust)
• Computational methods for HSCT-inlet controls/CFD interdisciplinary research / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994), by Gary L. Cole and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A computer program to improve STADAN station scheduling / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by Walter D. Davis and Goddard Space Flight Center (page images at HathiTrust)
• Transonic aerodynamic characteristics of a tailless fixed-wing supersonic transport model / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by Edward J. Ray, Robert T. Taylor, and Langley Research Center (page images at HathiTrust)

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