Rotor-shielding effect on fan-OGV broadband noise prediction
Author:
Affiliation:
1. University of Sherbrooke
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2878
Reference47 articles.
1. A reflection mechanism for aft fan tone noise from turbofan engines
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3. Trapped acoustic modes in aeroengine intakes with swirling flow
4. Fan Noise Source Diagnostic Test - Wall Measured Circumferential Array Mode Results
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1. Large Eddy Simulation of a scale-model turbofan for fan noise source diagnostic;22nd AIAA/CEAS Aeroacoustics Conference;2016-05-27
2. Effect of Rotor Shielding on Fan-Outlet Guide Vanes Broadband Noise Prediction;AIAA Journal;2013-07
3. On the use of an analytical cascade response function to predict sound transmission through an annular cascade;Journal of Sound and Vibration;2013-07
4. The acoustic analogy in an annular duct with swirling mean flow;Journal of Fluid Mechanics;2013-06-10
5. Acoustic analogy in swirling mean flow applied to predict rotor trailing-edge noise;18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference);2012-06-04
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