The Online Books Page

Books by William C. Sleeman:

Books in the extended shelves:

• Sleeman, William C.: Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section. Transonic-bump method (National Advisory Committee for Aeronautics, 1949), also by Robert E. Becht, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Sleeman, William C.: Aerodynamic characteristics of a wing with quarter-chord line swept back 35°, aspect ratio 6, taper ratio 0.6, and NACA 65A006 airfoil section. Transonic-bump method (National Advisory Committee for Aeronautics, 1949), also by William D. Morrison, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Sleeman, William C.: Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift. (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Sleeman, William C.: Low-speed effects of high-lift devices on the aerodynamic characteristics of a supersonic transport model with outboard tails (National Aeronautics and Space Administration, 1963), also by Paul G. Fournier, Edward J. Ray, and Langley Research Center (page images at HathiTrust)
• Sleeman, William C.: Low-speed investigation of cable tension and aerodynamic characteristics of a parawing and spacecraft combination (National Aeronautics and Space Administration :, 1963), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Sleeman, William C.: 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 A. Warner Robins and Langley Research Center (page images at HathiTrust)
• Sleeman, William C.: Low-speed longitudinal characteristics of a airplane configuration including effects of canard and wing trailing-edge flap controls in combination (National Aeronautics and Space Administration :, 1962), also by Bernard Spencer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Sleeman, William C.: Low-speed wind-tunnel investigation of a four-engine upper surface blown model having a swept wing and rectangular and D-shaped exhaust nozzles (National Aeronautics and Space Administration ;, 1975), also by William C. Hohlweg and Langley Research Center (page images at HathiTrust)
• Sleeman, William C.: Low-speed wind-tunnel investigation of a swept-wing model having distributed upper-surface blowing near the wing leading edge or at the flap knee (National Aeronautics and Space Administration ;, 1977), also by Langley Research Center, United States National Aeronautics and Space Administration, and David R Forsyth (page images at HathiTrust)
• Sleeman, William C.: NASA TN D-4010 (National Aeronautics and Space Administration ;, 1967), also by Frank M. Bugg, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Sleeman, William C.: NASA TN D-5974 (National Aeronautics and Space Administration :, 1970), also by Paul G. Fournier, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Sleeman, William C.: The rolling moment due to sideslip of swept wings at subsonic and transonic speeds (National Aeronautics and Space Administration, 1960), also by Edward C. Polhamus (page images at HathiTrust)
• Sleeman, William C.: The rolling moment due to sideslip of swept wings at subsonic and transonic speeds (National Advisory Committee for Aeronautics, 1955), also by Edward C. Polhamus, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Sleeman, William C.: Wing-surface-jet interaction characteristics of an upper-surface blown model with rectangular exhaust nozzles and a radius flap (National Aeronautics and Space Administration ;, 1976), also by Alvin M. Bloom, William C. Hohlweg, and United States National Aeronautics and Space Administration (page images at HathiTrust)

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