Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2
By: E. Ann Bare and David E. Reubush, Raymond C. Haddad.
Contributors: Reubush, David E.; Haddad, Raymond C.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program
Series: NASA technical memorandum -- 4296
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; For sale by the National Technical Information Service]
Published: 1992
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Airplanes -- Wings, Triangular.; Leading edges (Aerodynamics)
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 92-1811-M.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1992. 2 microfiches.