The Online Books Page

Trailing edges

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• Large-scale static investigation of circulation-control-wing concepts applied to upper-surface-blowing aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987), by M. D. Shovlin and Ames Research Center (page images at HathiTrust)
• Low-speed aerodynamic characteristics of airfoil sections with rounded trailing edges in forward and reverse flow (National Aeronautics and Space Administration ;, 1974), by William D. Beasley, Robert J. McGhee, and Langley Research Center (page images at HathiTrust)
• Experimental investigation in an annular cascade sector of highly loaded turbine stator blading. Volume IV, Performance of jet-flapped blade (National Aeronautics and Space Administration ;, 1969), by James L. Bettner, Lewis Research Center, and General Motors Corporation (page images at HathiTrust)
• Experimental investigation of advanced concepts to increase turbine blade loading. III, Performance evaluation of tandem rotor blade (National Aeronautics and Space Administration ;, 1968), by H. G. Lueders, General Motors Corporation. Allison Division, and Lewis Research Center (page images at HathiTrust)
• Pressure distributions and aerodynamic characteristics of several spoiler controls on a 40 degree sweptback wing at a Mach number of 1.61 (National Aeronautics and Space Administration, 1960), by Emma Jean Landrum, K. R. Czarnecki, and Langley Research Center (page images at HathiTrust)
• Free-flight investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on an 80° delta-wing missile (National Aeronautics and Space Administration, 1960), by Eugene D. Schult and Langley Research Center (page images at HathiTrust)
• Measured and theoretical flow fields behind a rectangular and a triangular wing up to high angles of attack at a Mach number of 2.46 (National Aeronautics and Space Administration, 1959), by Frank J. Centolanzi and Ames Research Center (page images at HathiTrust)
• Low subsonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading-edge sweep (National Aeronautics and Space Administration, 1961), by Paul G. Fournier, B. Ann Bell, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)

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