The Online Books Page

Books by Bernard Spencer:

Books in the extended shelves:

• Spencer, Bernard, 1932-: Aerodynamic and flow-visualization studies of variations in the geometry of irregular planform wings at a Mach number of 20.3 (National Aeronautics and Space Administration ;, 1974), also by David R. Stone and Langley Research Center (page images at HathiTrust)
• Spencer, Bernard, 1932-: Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Delma C. Freeman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Spencer, Bernard, 1932-: Effects of canard planform and wing-leading-edge modification on low-speed longitudinal aerodynamic characteristics of a canard airplane configuration (National Aeronautics and Space Administration, 1961), also by United States National Aeronautics and Space Administration and Langley Research Center (page images at HathiTrust)
• Spencer, Bernard, 1932-: High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0 degree to 90 degree (National Aeronautics and Space Administration, 1959), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Spencer, Bernard, 1932-: An investigation at subsonic speeds of aerodynamic charactersitcs at angles of attack from -4⁰ to 100⁰ of a delta-wing reentry configuration having folding wingtip panels (National Aeronautics and Space Administration, Langley Research Center, 1960), also by Langley Research Center (page images at HathiTrust)
• Spencer, Bernard, 1932-: Low-speed aerodynamic charachteristics of a cargo airplane configuration having split flaps located ahead of the wing trailing edge and leading- and trailing-edge flaps on the Canard Control. Bernard Spencer Jr. (National Aeronautics and Space Administration :, 1962), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Spencer, Bernard, 1932-: NASA TN D-1963 (National Aeronautics and Space Administration, 1963), also by W. Pelham Phillips, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Spencer, Bernard, 1932-: NASA TN D-2033 (National Aeronautics and Space Administration, 1963), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Spencer, Bernard, 1932-: NASA TN D-4079 (National Aeronautics and Space Administration ;, 1967), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Spencer, Bernard, 1932-: NASA TR R-250 (National Aeronautics and Space Administration ;, 1966), also by Charles H. Fox, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Spencer, Bernard, 1932-: Stability and control characteristics at low subsonic speeds of an airplane configuration having two types of variable-sweep wings (National Aeronautics and Space Administration, 1960), also by Langley Research Center (page images at HathiTrust)

Find more by Bernard Spencer at your library, or elsewhere.