preliminary assessment of the impact of 2-D exhaust-nozzle geometry on the cruise range of a hypersonic aircraft with top-mounted ramjet propulsion
By: Walter A. Vahl and John P. Weidner
Contributors: Weidner, John P. 1938-; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center (U.S.)
Series: NASA technical memorandum -- 81841
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: 57
Subjects: Aerodynamics, Hypersonic; Jet propulsion
Notes: "Langley Research Center."

Sept. 1980

Includes bibliographical references