Books by A. Warner Robins:
Books in the extended shelves:
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Robins, A. Warner: Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by David S. Miller, Milton Lamb, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)- Robins, A. Warner: Characteristics at mach number of 2.03 of a series of wings having various spanwise distributions of thickness ration and chord (National Aeronautics and Space Administration :, 1960), also by Charlie M. Jackson, Roy V. Harris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Robins, A. Warner: Concept development of a Mach 3.0 high-speed civil transport (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
- Robins, A. Warner: The effect of nose radius and shape of the aerodynamic characteristics of a fuselage and a wing-fuselage combination at angles of attack (National Advisory Committee for Aeronautics, 1953), also by John P. Gapcynski, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- Robins, A. Warner: Longitudinal aerodynamic characteristics of an elliptical body with a horizontal tail at mach numbers 2.3 to 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Barrett L. Shrout, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
- Robins, A. Warner: Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body (National Aeronautics and Space Administration, 1961), also by William C. Sleeman and Langley Research Center (page images at HathiTrust)
- Robins, A. Warner: Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60 (National Advisory Committee for Aeronautics, 1958) (page images at HathiTrust)
- Robins, A. Warner: Supersonic wings with significant leading-edge thrust at cruise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Robert J. Mack, Harry W. Carlson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Robins, A. Warner: The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack (National Aeronautics and Space Administration, 1960), also by Ralph P. Bielat, William J. Alford, and Langley Research Center (page images at HathiTrust)
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