The Online Books Page

Books by Dennis E. Fuller:

Books in the extended shelves:

• Fuller, Dennis E.: Aerodynamic characteristics of a fixed arrow-wing supersonic cruise aircraft at Mach numbers of 2.30, 2.70, and 2.95 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Odell A. Morris, Crolyn B. Watson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Fuller, Dennis E.: Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing (National Aeronautics and Space Administration, 1964), also by Odell A. Morris and Langley Research Center (page images at HathiTrust)
• Fuller, Dennis E.: Description of 0.186-scale model of high-speed duct of national transonic facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Garl L. Gentry, William B. Igoe, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Fuller, Dennis E.: Effect of afterbody geometry and sting diameter on the aerodynamic characteristics of slender bodies at Mach number from 1.57 to 2.86 (National Aeronautics and Space Administration :, 1963), also by Victor E. Langhans and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fuller, Dennis E.: Effect of cross-section shape on the aerodynamics characteristics of bodies at Mach numbers from 2.50 to 4.63 (National Aeronautics and Space Administration :, 1963), also by Donald L. Wassum, David S. Shaw, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fuller, Dennis E.: Guide for users of the National Transonic Facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Fuller, Dennis E.: NASA TN D-1781 (National Aeronautics and Space Administration ;, 1963), also by David S. Shaw, C. Donald Babb, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fuller, Dennis E.: NASA TN D-2352 (National Aeronautics and Space Administration :, 1964), also by Roger H. Fournier, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fuller, Dennis E.: NASA TN D-4014 (National Aeronautics and Space Administration ;, 1967), also by C. Donald Babb, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fuller, Dennis E.: Pressure distributions for a rectangular supersonic inlet at subsonic speeds (National Aeronautics and Space Administration ;, 1976), also by Langley Research Center (page images at HathiTrust)
• Fuller, Dennis E.: Static aerodynamic characteristics of three rocket-vehicle configurations at Mach numbers from 1.80 to 4.63 including some effects of fin size, fin cant, and auxiliary rocket motors (National Aeronautics and Space Administration, 1963), also by Gerald V. Foster and Langley Research Center (page images at HathiTrust)
• Fuller, Dennis E.: Static stability investigations of proposed project fire space-vehicle and reentry-package configurations at Mach numbers from 1.47 to 4.63 (National Aeronautics and Space Administration :, 1962), also by C. Donald Babb and United States National Aeronautics and Space Administration (page images at HathiTrust)

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