Books by Michael J. Mann:
Books in the extended shelves:
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Mann, Michael J.: Aerodynamic design for improved maneuverability by use of three-dimensional transonic theory (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by James C. Ferris, Richard L. Campbell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)- Mann, Michael J.: Calculation of the twist distribution of wings designed for cruise at transonic speeds (National Aeronautics and Space Administration ;, 1974), also by Langley Research Center (page images at HathiTrust)
- Mann, Michael J.: The design of supercritical wings by the use of three-dimensional transonic theory (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Mann, Michael J.: Experimental study of wing leading-edge devices for improved maneuver performance of a supercritical maneuvering fighter configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Mann, Michael J.: Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Charles E. Mercer and Langley Research Center (page images at HathiTrust)
- Mann, Michael J.: Low-speed upwash interference on a transport model in a rectangular slotted-wall wind tunnel (National Aeronautics and Space Administration ;, 1975), also by Langley Research Center (page images at HathiTrust)
- Mann, Michael J.: Subsonic annular wing theory with application to flow about nacelles (National Aeronautics and Space Administration ;, 1974), also by Langley Research Center (page images at HathiTrust)
- Mann, Michael J.: Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47⁰ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Charles H. Fox, Jarrett K. Huffman, and Langley Research Center (page images at HathiTrust)
- Mann, Michael J.: Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Richard L. Campbell, Charles E. Mercer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Mann, Michael J.: Theoretical estimation of the transonic aerodynamic characteristics of a supercritical-wing transport model with trailing-edge controls (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by James M. Luckring, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Mann, Michael J.: Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Harry W. Carlson, Christine M. Darden, and Langley Research Center (page images at HathiTrust)
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