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Experimental aerodynamic characteristics at Mach numbers from 0.60 to 2.70 of two supersonic cruise fighter configurations /
Samuel M. Dollyhigh.

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Main Author: Dollyhigh, Samuel M.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; 1979.
Subjects: Fighter planes > Fighter planes / Design and construction.
Supersonic wind tunnels.
Aerodynamics, Supersonic.
Note: Feb. 1979.
"Langley Research Center, Hampton, Virginia."
Physical Description: 187 p. : ill. ; 27 cm.
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