The Online Books Page

Lift drag ratio

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• Flight test results pertaining to the Space Shuttlecraft : a symposium held at Flight Research Center, Edwards, Calif., June 30, 1970. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by Flight Research Center (U.S.) (page images at HathiTrust)
• Effects of a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Emma Jean Landrum and Langley Research Center (page images at HathiTrust)
• Lift and drag characteristics at subsonic speeds and at a Mach number of 1.9 of a lifting circular cylinder with a fineness ratio of 10 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Vernard E. Lockwood, Linwood W. McKinney, and Langley Research Center (page images at HathiTrust)
• Importance of the variation of drag with lift in minimization of satellite entry acceleration / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Frederick C. Grant and Langley Research Center (page images at HathiTrust)
• Fundamental limitations on V/STOL terminal guidance due to aircraft characteristics / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1971), by Julian Wolkovitch, D. William Lochtie, Charles W. LaMont, Lewis Research Center, and inc Mechanics Research (page images at HathiTrust)
• Effect of ground proximity on the aerodynamic characteristics of aspect-ratio-1 airfoils with and without end plates / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Arthur W. Carter, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• The variation and control of range traveled in the atmosphere by a high-drag variable-lift entry vehicle / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Donald C. Cheatham, John M. Eggleston, John W. Young, and Langley Research Center (page images at HathiTrust)
• Stability and control characteristics of a monoplanar missile configuration with two low-profile tail arrangements at Mach numbers from 1.70 to 2.86 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by A. B. Blair and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Consideration of some aerodynamic characteristics during take-off and landing of jet airplanes / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by John M. Riebe and Langley Research Center (page images at HathiTrust)

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