Books by Jimmy L. Pittman:
Books in the extended shelves:
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Pittman, Jimmy L.: Aeordynamic characteristics of a distinct wing-body configuration at Mach 6 : experiment, theory, and the hypersonic isolation principle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Jim A. Penland and Langley Research Center (page images at HathiTrust)- Pittman, Jimmy L.: Aerodynamic characteristics at Mach 6 of a wing-body concept for a hypersonic research airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by James L. Dillon, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Pittman, Jimmy L.: Aerodynamic characteristics at Mach numbers from 0.33 to 1.20 of wing-body design concept for a hypersonic research airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by James L. Dillon and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Pittman, Jimmy L.: Aerodynamic characteristics of a hypersonic cruise aircraft concept with wing-mounted propulsion systems at mach numbers of 2.96, 3.96, and 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Gregory D. Riebe, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Pittman, Jimmy L.: Application of supersonic linear theory and hypersonic impact methods to three nonslender hypersonic airplane concepts at mach numbers from 1.10 to 2.86 (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)
- Pittman, Jimmy L.: Body and canard effects on an attached-flow maneuver wing at Mach 1.62 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by William H. Mason, David S. Miller, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Pittman, Jimmy L.: Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Gregory D. Riebe, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
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