Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

An edition of Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control (1999)

Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

By Scott C. Asbury

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Publish Date

1999

Publisher

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

Language

eng

Pages

Description:

subjects: Cavities, Exhaust nozzles, Hole geometry (Mechanics), Porosity, Thrust vector control