Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63
By: Jimmy L. Pittman and Gregory D. Riebe
Contributors: Riebe, Gregory D; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical paper -- 1767
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1980
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Number of pages: 113
Subjects: Aerodynamics, Supersonic; Hypersonic planes; Supersonic wind tunnels; Mach number
Notes: "Langley Research Center."

Dec. 1980

Includes bibliographical references