The Online Books Page

Online Books by

William J. Alford

Books from the extended shelves:

• Alford, William J.: Aerodynamic-center considerations of wings and wing-body combinations (National Aeronautics and Space Administration :, 1966), also by John E. Lamar and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Alford, William J.: Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds (National Advisory Committee for Aeronautics, 1956), also by Frank S. Malvestuto, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Alford, William J.: Experimental aerodynamic forces and moments at low speed of a missile model during simulated launching from the midsemispan location of a 45 degree sweptback wing-fuselage combination (Washington, D.C. : National Advisory Committee for Aeronautics, [1955], 1955), also by Thomas J. King, H. Norman Silvers, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Alford, William J.: Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers of 0.40 to 0.93 of a 45° sweptback wing of aspect ratio 4 (National Advisory Committee for Aeronautics, 1957), also by Kenneth P. Spreemann, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Alford, William J.: Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep (National Aeronautics and Space Administration, 1960), also by Arvo A. Luoma, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Alford, William J.: Subsonic wind-tunnel investigation of errors indicated by total-pressure tubes in the flow field of a body simulating the nose of the X-15 research airplane. William J. Alford Jr. (National Aeronautics and Space Administration :, 1962), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Alford, William J.: A technique for firing dynamically scaled missile models in wind tunnels and for measuring rocket-motor sound and pressure fluctuations (National Aeronautics and Space Administration, 1960), also by Kenneth W. Goodson (page images at HathiTrust)
• Alford, William J.: Theoretical and experimental investigation of the subsonic-flow fields beneath swept and unswept wings with tails of vortex-induced velocities (National Advisory Committee for Aeronautics, 1956), also by United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Alford, William J.: 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, A. Warner Robins, and Langley Research Center (page images at HathiTrust)
• Alford, William J.: Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration (National Aeronautics and Space Administration, 1959), also by William P. Handerson, Arvo A. Luoma, and Langley Research Center (page images at HathiTrust)

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