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

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

-

1-1 of 1 Editions

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

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

Language: eng

Published In: 1994

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