Boundary layer transitionSee also what's at your library, or elsewhere.
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Filed under: Boundary layer transition A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layers / ([Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1992]), by Z. Yang, T. H. Shih, and United States National Aeronautics and Space Administration (page images at HathiTrust) Supersonic free-flight measurements of heat transfer and transition on a 10° cone having a low temperature ratio / (Washington, [D.C.] : National Aeronautical and Space Administration, 1961), by Charles F. Merlet, Charles B. Rumsey, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust) A viscous/potential flow interaction analysis method for multi-element infinite swept wings. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by F. A. Dvorak, F. A. Woodward, and inc Flow Research (page images at HathiTrust) Evolution of amplified waves leading to transition in a boundary layer with zero pressure gradient / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by P. S. Klebanoff, K. D. Tidstrom, and United States. National Bureau of Standards (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 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Louis S. Stivers and Ames Research Center (page images at HathiTrust) Effect of distributed three-dimensional roughness and surface cooling on boundary-layer transition and lateral spread of turbulence at supersonic speeds / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Albert L. Braslow, Elmer A. Horton, Eugene C. Know, and Langley Research Center (page images at HathiTrust) Two techniques for detecting boundary-layer transition in flight at supersonic speeds and at altitudes above 20,000 feet / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by John G. McTigue, Gilbert Petty, John D. Overton, and Flight Research Center (U.S.) (page images at HathiTrust)
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