AIRFOIL GUST RESPONSE AND THE SOUND PRODUCED BY AIRFOIL-VORTEX INTERACTION
Author:
Affiliation:
1. UNITED TECHNOLOGIES RESEARCH CENTER, EAST HARTFORD, CT
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1984-2268
Reference30 articles.
1. Figure 9 Process. The only difference in these curves is in the location af the observer. For different observer positions the phasing of the sources on the airfoil will be different because of differences in propagation times.
2. I I -0.2 I
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1. Experimental and Numerical Investigation of Turbulence-Airfoil Noise Reduction Using Wavy Edges;AIAA Journal;2013-11
2. CAA methodology to simulate turbulence-airfoil noise;18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference);2012-06-04
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