Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept

An edition of Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept (1994)

Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept

By David J. Wing

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Publish Date

1994

Publisher

National Aeronautics and Space Administration, Langley Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Testing, Sonic nozzles, Exhaust nozzles, Jet nozzles, Wind tunnel tests, Nozzle geometry, Static tests, Throats, Skewness, Thrust vector control