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

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

Bibliographic Details
Main Author: Bare, E. Ann
Corporate Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Program
Other Authors: Reubush, David E., Haddad, Raymond C.
Format: Government Document Book
Language:English
Published: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; 1992.
Series:NASA technical memorandum ; 4296.
Subjects:
Airplanes > Wings, Triangular.
Leading edges (Aerodynamics)

Evans: US Documents Microfiche (3rd floor)

Holdings details from Evans: US Documents Microfiche (3rd floor)
Call Number: NAS 1.15:4296
 
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NAS 1.15:4296 Available