Last edited by Gardagul
Wednesday, July 29, 2020 | History

3 edition of Preliminary in-flight boundary layer transition measurements on a 45-degree swept wing at Mach numbers between 0.9 and 1.8 found in the catalog.

Preliminary in-flight boundary layer transition measurements on a 45-degree swept wing at Mach numbers between 0.9 and 1.8

Preliminary in-flight boundary layer transition measurements on a 45-degree swept wing at Mach numbers between 0.9 and 1.8

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Published by National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility in Edwards, Calif .
Written in English

    Subjects:
  • Laminar flow.

  • Edition Notes

    StatementJ. Blair Johnson.
    SeriesNASA technical memorandum -- 100412.
    ContributionsDryden Flight Research Facility.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15278262M


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Preliminary in-flight boundary layer transition measurements on a 45-degree swept wing at Mach numbers between 0.9 and 1.8 Download PDF EPUB FB2