Aerodynamic characteristics of a hypersonic cruise aircraft concept with wing-mounted propulsion systems at mach numbers of 2.96, 3.96, and 4.63
By: Gregory D. Riebe and Jimmy L. Pittman
Contributors: Pittman, Jimmy L; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical memorandum -- 81937
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1981
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 48
Subjects: Aerodynamics
Notes: "Langley Research Center."

"March 1981"--Cover

Subject category 02