Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2
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Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2

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Published by National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, For sale by the National Technical Information Service] in [Washington, DC], [Springfield, Va .
Written in English

Subjects:

  • Airplanes -- Wings, Triangular.,
  • Leading edges (Aerodynamics)

Book details:

Edition Notes

StatementE. Ann Bare and David E. Reubush, Raymond C. Haddad.
SeriesNASA technical memorandum -- 4296.
ContributionsReubush, David E., Haddad, Raymond C., United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL17675057M

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