The Online Books Page

Lift

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• Low speed aerodynamic characteristics of NACA 6716 and NACA 4416 airfoils with 35 percent-chord single-slotted flaps (National Aeronautics and Space Administration ;, 1974), by Gene J. Bingham, Kevin W. Noonan, and Langley Research Center (page images at HathiTrust)
• Effects of a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 (National Aeronautics and Space Administration, 1960), by Emma Jean Landrum and Langley Research Center (page images at HathiTrust)
• Effectiveness of an all-movable horizontal tail on an unswept-wing and body combination for Mach numbers from 0.60 to 1.40 (National Aeronautics and Space Administration, 1959), by Louis S. Stivers and Ames Research Center (page images at HathiTrust)
• Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing, four propellers, and blowing flaps (National Aeronautics and Space Administration, 1959), by James A. Weiberg, V. Robert Page, and Ames Research Center (page images at HathiTrust)
• A method for longitudinal and lateral range control for a high-drag low-lift vehicle entering the atmosphere of a rotating earth (National Aeronautics and Space Administration, 1961), by John W. Young, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Investigation of aerodynamic effects of external combustion below flat-plate model in 10- by 10-foot wind tunnel at Mach 2.4 (National Aeronautics and Space Administration, 1960), by Robert G. Dorsch, Murray Dryer, Harrison Allen, and Lewis Research Center (page images at HathiTrust)
• Compressibility effects on the hovering performance of a two-blade 10-foot-diameter helicopter rotor operating at tip Mach numbers up to 0.98 (National Aeronautics and Space Administration, 1960), by Joesph W. Jewel and Langley Research Center (page images at HathiTrust)
• Lift generation on a circular cylinder by tangential blowing from surface slots (National Aeronautics and Space Administration, 1960), by Vernard E. Lockwood and Langley Research Center (page images at HathiTrust)
• Experimental investigation at a Mach number of 3.11 of the lift, drag, and pitching-moment characteristics of five blunt lifting bodies (National Aeronautics and Space Administration, 1960), by William Letko and Langley Research Center (page images at HathiTrust)
• Lift and drag characteristics at subsonic speeds and at a Mach number of 1.9 of a lifting circular cylinder with a fineness ratio of 10 (National Aeronautics and Space Administration, 1959), by Vernard E. Lockwood, Linwood W. McKinney, and Langley Research Center (page images at HathiTrust)
• Flight investigation of an automatic pitchup control (National Aeronautics and Space Administration, 1960), by George J. Hurt, James B. Whitten, and Langley Research Center (page images at HathiTrust)
• Importance of the variation of drag with lift in minimization of satellite entry acceleration (National Aeronautics and Space Administration, 1959), by Frederick C. Grant and Langley Research Center (page images at HathiTrust)
• Full-scale wind-tunnel tests of a low-aspect-ratio, straight-wing airplane with blowing boundary-layer control on leading- and trailing-edge flaps (National Aeronautics and Space Administration, 1959), by Mark W. Kelly, Ralph L. Maki, William H. Tolhurst, and Ames Research Center (page images at HathiTrust)
• Effect of groundboard height on the aerodynamic characteristics of a lifting circular cylinder using tangential blowing from surface slots for lift generation (National Aeronautics and Space Administration, 1961), by Vernard E. Lockwood, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Low-speed wind-tunnel investigation of blowing boundary-layer control on leading- and trailing-edge flaps of a full-scale, low-aspect-ratio, 42° swept-wing airplane configuration (National Aeronautics and Space Administration, 1959), by Ralph L. Maki, Demo J. Giulianetti, and Ames Research Center (page images at HathiTrust)
• Flight investigation of the lift and drag characteristics of a swept-wing, multijet, transport-type airplane (National Aeronautics and Space Administration, 1960), by Ronald Tambor and Flight Research Center (U.S.) (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.