Last edited by Tauzragore
Sunday, April 26, 2020 | History

3 edition of Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds found in the catalog.

Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds

Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds

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Published by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va .
Written in English

    Subjects:
  • Guided missiles -- Aerodynamics.,
  • Angle of attack.,
  • Euler equations of motion.,
  • Missile configurations.,
  • Pressure distribution.,
  • Supersonic flow.,
  • Transonic flow.,
  • Wind tunnel models.,
  • Wind tunnel tests.

  • Edition Notes

    StatementPatsy S. Fulton.
    SeriesNASA technical memorandum -- 101531.
    ContributionsLangley Research Center.
    The Physical Object
    FormatMicroform
    Paginationvi, 115 p.
    Number of Pages115
    ID Numbers
    Open LibraryOL15407176M


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Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds Download PDF EPUB FB2