Advanced turboprop wing installation effects measured by unsteady blade pressure and noise

An edition of Advanced turboprop wing installation effects measured by unsteady blade pressure and noise (1987)

Advanced turboprop wing installation effects measured by unsteady blade pressure and noise

By Laurence J. Heidelberg

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Publish Date

1987

Publisher

National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Wings, Turboprop engines, Unsteady flow, Pressure distribution, Propellers, Airplanes, Installing, Engine noise, Compressor blades