Acoustics and thrust of separate-flow exhaust nozzles with mixing devices for high-bypass-ratio engines
Author:
Affiliation:
1. NASA, Glenn Research Center, Cleveland, OH
2. Aero Systems Engineering, Saint Paul, MN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-1961
Reference19 articles.
1. Aircraft Turbofan Noise
2. Aircraft Noise
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