Experimental aerodynamic characteristics at Mach numbers from 0.60 to 2.70 of two supersonic cruise fighter configurations
By: Samuel M. Dollyhigh.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.; Langley Research Center.
Series: NASA technical memorandum -- 78764.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1979
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 187
Subjects: Aerodynamics, Supersonic.; Supersonic wind tunnels.; Fighter planes -- Design and construction.
Notes: "Langley Research Center, Hampton, Virginia."

Feb. 1979.