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

2 edition of Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing found in the catalog.

Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing

Thomas A Byrdsong

Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing

by Thomas A Byrdsong

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  • 6 Currently reading

Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English

    Subjects:
  • Wind tunnels,
  • Aerodynamic load,
  • Airplanes -- Wings

  • Edition Notes

    StatementThomas A. Byrdsong and Cuyler W. Brooks, Jr
    SeriesNASA technical memorandum -- 84614
    ContributionsBrooks, Cuyler W, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
    The Physical Object
    Pagination211 p. :
    Number of Pages211
    ID Numbers
    Open LibraryOL17977366M


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Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing by Thomas A Byrdsong Download PDF EPUB FB2