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



Publisher: National Aeronautics and Space Administration, Langley Research Center, Publisher: National Technical Information Service, distributor in Hampton, Va, [Springfield, Va

Written in English
Published: Pages: 115 Downloads: 60
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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

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