Inlet geometry and axial Mach number effects on fan noise propagation
Author:
Affiliation:
1. United Aircraft Corp., Pratt and Whitney Aircraft Div., East Hartford, Conn.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1973-1022
Reference8 articles.
1. On the Attenuation of a Repeated Sawtooth Shock Wave
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