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More about Albert L. Braslow:
| | Books by Albert L. Braslow: Books in the extended shelves: Braslow, Albert L.: Analysis of boundary-layer transition on X-15-2 research airplane (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1966) (page images at HathiTrust) Braslow, Albert L.: Effect of distributed three-dimensional roughness and surface cooling on boundary-layer transition and lateral spread of turbulence at supersonic speeds (National Aeronautics and Space Administration, 1959), also by Elmer A. Horton, Eugene C. Know, and Langley Research Center (page images at HathiTrust) Braslow, Albert L.: An experimental study of a method of designing the sweptback-wing - fuselage juncture for reducing the drag at transonic speeds (National Advisory Committee for Aeronautics, 1955), also by Robert R. Howell, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Braslow, Albert L.: History of suction type laminar flow control with emphasis on flight research (NASA History Office, Office of Policy and Plans, NASA Headquarters, 1999), also by United States. National Aeronautics and Space Administration. Office of Policy and Plans (page images at HathiTrust) Braslow, Albert L.: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by William J. Underwood, Jones F. Cahill, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust) Braslow, Albert L.: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by United States National Advisory Committee for Aeronautics and Langley Aeronautical Laboratory (page images at HathiTrust) Braslow, Albert L.: Ordinates and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively (U.S. G.P.O., 1961), also by Elizabeth W. Patterson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust) Braslow, Albert L.: A rigidly forced oscillation system for meaasuring dynamic-stability parameters in transonic and supersonic wind tunnels (National Aeronautics and Space Administration :, 1962), also by Cullen Q. Lee, Harleth G. Wiley, and United States National Aeronautics and Space Administration (page images at HathiTrust) Braslow, Albert L.: Simulated-airline-service flight tests of laminar flow control with perforated-surface suction system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Dal V. Maddalon and Langley Research Center (page images at HathiTrust) Braslow, Albert L.: Studies of the use of Freon-12 as a testing medium in the Langley low-turbulence pressure tunnel (National Advisory Committee for Aeronautics, 1951), also by Albert E. Von Doenhoff, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust) Braslow, Albert L.: Subsonic investigation of effects of body indentation on zero-lift drag characteristics of a 45° sweptback wing-body combination with natural and fixed boundary-layer transition through a range of Reynolds number from 1 x 10⁶ to 8 x 10⁶ (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), also by Gene J. Bingham, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Braslow, Albert L.: Transonic investigation at lifting conditions of streamline contouring in the sweptback-wing-fuselage juncture in combination with the transonic area rule (National Advisory Committee for Aeronautics, 1956), also by William E. Palmer, Robert R. Howell, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
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