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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 /
E. Ann Bare and David E. Reubush, Raymond C. Haddad.



Main Author: Bare, E. Ann.
Related Names: Haddad, Raymond C. , Reubush, David E.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Subjects: Fighter planes.
Flaps (Airplanes)
Leading edges (Aerodynamics)
Airplanes > Airplanes / Control systems.
Airplanes > Airplanes / Wings, Triangular.
Note: Prepared at Langley Research Center.
Physical Description: iv, 121 p. : ill. ; 28 cm.
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