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Exhaust-nozzle characteristics for a twin-jet variable-wing-sweep fighter airplane model at Mach numbers to 2.2 /
by David E. Reubush and Charles E. Mercer.

Description

Tools

Main Author: Reubush, David E.
Related Names: Mercer, Charles E.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; 1974.
Subjects: Fighter planes.
Drag (Aerodynamics)
Exhaust nozzles.
Note: Prepared at Langley Research Center.
Cover title.
Physical Description: 135 p. : ill. ; 27 cm.
Locate a Print Version: Find in a library

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Full view University of Illinois at Urbana-Champaign
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