Last edited by Mektilar
Wednesday, May 13, 2020 | History

3 edition of Development of a temperature-compensated hot-film anemometer system for boundary-layer transition detection of high performance aircraft found in the catalog.

Development of a temperature-compensated hot-film anemometer system for boundary-layer transition detection of high performance aircraft

Development of a temperature-compensated hot-film anemometer system for boundary-layer transition detection of high performance aircraft

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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:
  • Transition flow.,
  • Aeronautical instruments.

  • Edition Notes

    StatementHarry R. Chiles and J. Blair Johnson.
    SeriesNASA technical memorandum -- 86732.
    ContributionsJohnson, J. Blair., Dryden Flight Research Facility.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL17658801M


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