The Online Books Page

Books by Edwin J. Saltzman:

Books in the extended shelves:

• Saltzman, Edwin J.: Comparison of full-scale lift and drag characteristics of the x-15 airplane with wind-tunnel results and theory (National Aeronautics and Space Administration, 1962), also by Edward J. Hopkins, David E. Fetterman, Flight Research Center (U.S.), Langley Research Center, and Ames Research Center (page images at HathiTrust)
• Saltzman, Edwin J.: Flight evaluation of splitter-plate effectiveness in reducing base drag at Mach numbers from 0.65 to 0.90 (National Aeronautics and Space Administration ;, 1967), also by John Hintz and Flight Research Center (U.S.) (page images at HathiTrust)
• Saltzman, Edwin J.: Flight techniques for determining airplane drag at high Mach numbers (National Advisory Committee for Aeronautics, 1956), also by De E. Beeler, Donald R. Bellman, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Saltzman, Edwin J.: NASA TN D-2420 (National Aeronautics and Space Administration :, 1964), also by United States National Aeronautics and Space Administration and Flight Research Center (U.S.) (page images at HathiTrust; US access only)
• Saltzman, Edwin J.: NASA TN D-3830 (National Aeronautics and Space Administration :, 1967), also by Darwin J. Garringer and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Saltzman, Edwin J.: NASA TN D-5838 (National Aeronautics and Space Administration ;, 1970), also by David F. Fisher, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Saltzman, Edwin J.: NASA TN D-6428 (National Aeronautics and Space Administration ;, 1971), also by Flight Research Center (U.S.) and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Saltzman, Edwin J.: Preliminary base pressures obtained from the X-15 airplane at mach numbers from 1.1 to 3.2 (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Saltzman, Edwin J.: Preliminary full-scale power-off drag of the X-15 airplane for mach numbers from 0.7 to 3.1 (National Aeronautics and Space Administration, 1960), also by United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

Find more by Edwin J. Saltzman at your library, or elsewhere.