Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations

An edition of Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations (2001)

Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations

By Kevin L. Mikkelsen

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Publish Date

2001

Publisher

National Aeronautics and Space Administration, Glenn Research Center,Available from NASA Center for Aerospace Information

Language

eng

Pages

Description:

subjects: Wind tunnel tests, Cold flow tests, Pressure ratio static tests, Power efficiency, Nozzle flow