Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2 /
Francis J. Capone ; Langley Research Center, Hampton, Va.

Description

Main Author

Capone, Francis J.

Related Names

Langley Research Center.

Language(s)

English

Published

Washington : U.S. National Aeronautics and Space Administration ; 1976.

Subjects

Nozzles > Nozzles / Testing.
Airplanes > Airplanes / Jet propulsion.

Note

Cover title.

Physical Description

[1], 205 p. : ill. ; 27 cm.

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