Simulation of pressure and temperature responses for the 20 inch supersonic wind tunnel

An edition of Simulation of pressure and temperature responses for the 20 inch supersonic wind tunnel (1990)

Simulation of pressure and temperature responses for the 20 inch supersonic wind tunnel

By Mark A. Motter

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Publish Date

1990

Publisher

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

Language

eng

Pages

Description:

subjects: Flow distribution, Temperature effects, Pressure effects, Computerized simulation, Supersonic wind tunnels