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

Description

Main Author: Dollyhigh, Samuel M.
Related Names: 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 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.
Locate a Print Version: Find in a library

Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign