A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92

An edition of A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 (1996)

A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92

By Richard J. Re

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Publish Date

1996

Publisher

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

Language

eng

Pages

Description:

subjects: Static pressure, Pressure distribution, Wind tunnel tests, Subsonic flow, Angle of attack, Engine inlets, Aircraft engines, Mach number