Last edited by Kijin
Friday, July 24, 2020 | History

3 edition of Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79 found in the catalog.

Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79

Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79

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Published by National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, For sale by the National Technical Information Service in Edwards, Calif, [Springfield, Va .
Written in English

    Subjects:
  • Laminar flow.,
  • Boundary layer transition.,
  • Flow distribution.,
  • Laminar flow.,
  • Mach number.,
  • Pressure distribution.,
  • Variable sweep wings.

  • Edition Notes

    StatementBianca Trujillo Anderson and Robert R. Meyer, Jr.
    SeriesNASA technical memorandum -- 101701.
    ContributionsMeyer, Robert R., Dryden Flight Research Facility.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL16123798M


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Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79 Download PDF EPUB FB2