Last edited by Targ
Monday, July 20, 2020 | History

3 edition of Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction found in the catalog.

Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction

Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction

final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95

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Published by Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin, National Aeronautics and Space Administration, National Technical Information Service, distributor in Austin, Tex, [Washington, DC, Springfield, Va .
Written in English

    Subjects:
  • Aerodynamic loads.,
  • Boundary layer control.,
  • Boundary layer separation.,
  • Corner flow.,
  • Hypersonic boundary layer.,
  • Shock wave interaction.,
  • Turbulent boundary layer.,
  • Unsteady flow.,
  • Vortex generators.

  • Edition Notes

    Other titlesControl and reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction.
    StatementDavid S. Dolling and J.W. Barter.
    SeriesNASA contractor report -- NASA CR-199334.
    ContributionsBarter, J. W., United States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL18088579M


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