The Online Books Page

Wing profiles

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 (National Aeronautics and Space Administration, 1959), by Fred A. Demele and Ames Research Center (page images at HathiTrust)
• Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by the free-oscillation method (National Aeronautics and Space Administration, 1960), by W. J. Tuovila, R. W. Hess, and Langley Research Center (page images at HathiTrust)
• Methods of calculating fundamental solutions of the wave equation, with tables (National Aeronautics and Space Administration, 1959), by William A. Mersman and Ames Research Center (page images at HathiTrust)
• Investigation at transonic speeds to determine lateral control effectiveness of blowing laterally over surfaces of 30° and 45° swept wings (National Aeronautics and Space Administration, 1959), by Alexander D. Hammond, Linwood W. McKinney, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of effect of ratio of wing chord to propeller diameter with addition of slats on the aerodynamic characteristics of tilt-wing VTOL configurations in the transition speed range (National Aeronautics and Space Administration, 1959), by Robert T. Taylor, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Measured and predicted section wave drag coefficients at a Mach number of 1.6 for a delta wing with two airfoil sections (National Aeronautics and Space Administration, 1959), by Frederick C. Grant and Langley Research Center (page images at HathiTrust)

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