The Online Books Page

Online Books by

William A. Corlett

Books from the extended shelves:

• Corlett, William A.: 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 Langley Research Center (page images at HathiTrust)
• Corlett, William A.: 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 Langley Research Center (page images at HathiTrust)
• Corlett, William A.: 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, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Corlett, William A.: Lateral directional stability characteristics at mach 2.3 to 3.5 of a supersonic transport model with various outboard vertical-tail locations (National Aeronautics and Space Administration ;, 1965), also by Langley Research Center (page images at HathiTrust)
• Corlett, William A.: Supersonic aerodynamic characteristics of a 1/6-scale model of the final two stages of the Argo D-4 four-stage rocket vehicle (National Aeronautics and Space Administration ;, 1965), also by Clyde Hayes and Langley Research Center (page images at HathiTrust)
• Corlett, William A.: Supersonic stability and control characteristics of a cruciform missile model with delta wings and aft tail fin controls (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Corlett, William A.: Surface pressure data for 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, Ida K. Collins, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

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