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Effect on empennage location on twin-engine afterbody/nozzle aerodynamic characteristics at Mach numbers from 0.6 to 1.2 /
Laurence D. Leavitt.

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Main Author: Leavitt, Laurence D.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1983.
Subjects: Fighter planes > Fighter planes / Flight testing
Air-engines
Note: Distributed to depository libraries in microfiche.
"May 1983"--Cover.
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Item Link Original Source
Full view University of Illinois at Urbana-Champaign
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