Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel

An edition of Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel (1998)

Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel

By Richard J. Re

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Publish Date

1998

Publisher

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

Language

eng

Pages

Description:

subjects: Static pressure, Supersonic speed, Bow waves, Bodies of revolution, Mach number, Supersonic transports, Shock waves