The Online Books Page

Wing loading

See also what's at your library, or elsewhere.

• The effects of an inverse-taper leading-edge flap on the aerodynamic loading characteristics of a 45° sweptback wing at Mach numbers to 0.90 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Fred A. Demele and Ames Research Center (page images at HathiTrust)
• Transonic aerodynamic loading characteristics of a wing-body-tail combination having 52.5° sweptback wing of aspect ratio 3 with conical wing camber and body indentation for a design Mach number [square root of] 2 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Marlowe D. Cassetti, William B. Igoe, Richard J. Re, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Take-off distances of a supersonic transport configuration as affected by airplane rotation during the take-off run / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Albert W. Hall, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• The variation and control of range traveled in the atmosphere by a high-drag variable-lift entry vehicle / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Donald C. Cheatham, John M. Eggleston, John W. Young, and Langley Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.