The Online Books Page

Books by William P. Henderson:

Books in the extended shelves:

• Henderson, William P.: Adam's dream, and two other miracle plays for children (C. Scribner's sons, 1909), also by Alice Corbin Henderson and Roy McWilliams (page images at HathiTrust)
• Henderson, William P.: Aerodynamic characteristics of a high-wing transport configuration with an over-the-wing Nacelle-pylon arrangement (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by William Kelly Abeyounis and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Henderson, William P.: The effect of canard and vertical tails on the aerodynamic characteristics of a model with a 59 ̊sweptback wing at a Mach number of 0.30 (National Aeronautics and Space Administration ;, 1974), also by Langley Research Center (page images at HathiTrust)
• Henderson, William P.: Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by James R. Burley and Langley Research Center (page images at HathiTrust)
• Henderson, William P.: Effect of wing pivot location on longitudinal aerodynamic characteristics of a variable-sweep wing having an M planform (National Aeronautics and Space Administration, 1964), also by Edward J. Ray and Langley Research Center (page images at HathiTrust)
• Henderson, William P.: Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Henderson, William P.: Effects of wing leading-edge radius and Reynolds number on longitudinal aerodynamic characteristics of highly swept wing-body configurations at subsonic speeds (National Aeronautics and Space Administration ;, 1976), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Henderson, William P.: Lateral-directional stability characteristics of a wing-fuselage configuration at angles of attack up to 44 ̊ (National Aeronautics and Space Administration ;, 1974), also by Jarrett K. Huffman and Langley Research Center (page images at HathiTrust)
• Henderson, William P.: Low-speed longitudinal stability characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot (National Aeronautics and Space Administration, 1961), also by Langley Research Center (page images at HathiTrust)
• Henderson, William P.: NASA TN D-1796 (National Aeronautics and Space Administration, 1964), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Henderson, William P.: Pressure distributions on a cambered wing-body configuration at subsonic Mach numbers (National Aeronautics and Space Administration ;, 1975) (page images at HathiTrust)
• Henderson, William P.: Some effects of nose bluntness and fineness ration on the static longitudinal aerodynamic characteristics of bodies of revolution at subsonic speeds (National Aeronautics and Space Administration :, 1961), also by William C. Hayes and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Henderson, William P.: Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45? (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Laurence D. Leavitt, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Henderson, William P.: Wind-tunnel investigation at Mach numbers from 1.60 to 2.86 of the static aerodynamic characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot (National Aeronautics and Space Administration, 1962), also by David S. Shaw and Langley Research Center (page images at HathiTrust)

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