Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /
Jimmy L. Pittman and Gregory D. Riebe.

Description

Main Author: Pittman, Jimmy L.
Related Names: Riebe, Gregory D.
Langley Research Center.
United States. National Aeronautics and Space Administration.
Language(s): English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1980.
Subjects: Mach number.
Supersonic wind tunnels.
Hypersonic planes.
Aerodynamics, Supersonic.
Note: Dec. 1980.
"Langley Research Center."
Physical Description: 113 p. : ill. ; 27 cm.
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Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign