Measurements of Interaction and Scattered Modes in a Mixed Bypass/Core Duct due to Multiple Rotating Source
Author:
Affiliation:
1. NASA Glenn Research Center
2. Honeywell International, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3003
Reference21 articles.
1. Hubbard,H.Harvey,editor,AeroacousticsofFlightVehicles:TheoryandPractice:Volume1,NASAReference Publication 1258, Vol 1, WRDC Technical Report 90-3052.
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3. Flow quality improvements in the NASA Lewis Research Center 9- by 15-Foot Low Speed Wind Tunnel
4. Propulsion Simulator for High Bypass Turbofan Performance Evaluation
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