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Tuesday, August 11, 2020 | History

3 edition of Exploratory study of in-plane streamline curvature effects on a turbulent boundary layer at a mach number of 3 found in the catalog.

Exploratory study of in-plane streamline curvature effects on a turbulent boundary layer at a mach number of 3

Exploratory study of in-plane streamline curvature effects on a turbulent boundary layer at a mach number of 3

final technical report, grant NAG-1-961 for the period January 27, 1989 - January 26, 1990

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Published by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC, Springfield, Va .
Written in English

    Subjects:
  • Turbulent boundary layer.

  • Edition Notes

    Other titlesExploratory study of in plane streamline curvature effects on a turbulent boundary layer at a mach number of 3.
    Statementby Seymour M. Bogdonoff.
    Series[NASA contractor report] -- NASA CR-193673.
    ContributionsUnited States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL14697014M


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Exploratory study of in-plane streamline curvature effects on a turbulent boundary layer at a mach number of 3 Download PDF EPUB FB2