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  • Hypersonic turbulent boundary-layer and free shear database [microform] / Gary S. Settles and Lori J. Dodson.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1994

  • Self-adaptive difference method for the effective solution of computationally complex problems of boundary layer theory [microform] / W. Schönauer ... [et al.].

    • Text
    • Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Turbulence measurements in hypersonic boundary layers using contant-temperature anemometry and Reynolds stress measurements in hypersonic boundary layers [microform] : final grant report / Eric F. Spina.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction [microform] : final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95 / David S. Dolling and J.W. Barter.

    • Text
    • Austin, Tex. : Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel [microform] / Glen P. Doggett and Ndaona Chokani.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel [microform] / Stephen P. Wilkinson.

    • Text
    • Reston, VA : American Institute of Astronautics and Aeronautics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results [microform] / Jim A. Penland and Richard Hawkins.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
    • 1997

  • On the instability of hypersonic flow past a flat plate [microform] / Nicholas Blackaby, Stephen Cowley, Philip Hall.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60955

  • Secondary instability of stationary crossflow vortices in Mach 6 boundary layer over a circular cone / Fei Li [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 2015.
    • 2015-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67293

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