Forcing level effects of internal acoustic excitation on the improvement of airfoil performance
Author:
Affiliation:
1. CSIST, Taichung, Taiwan, Republic of China
2. National Cheng Kung University, Tainan, Taiwan, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46252
Reference13 articles.
1. Influence of Sound upon Separated Flow over Wings
2. Control of flow separation by sound
3. Effect of acoustic excitation on the flow over a low- Re airfoil
4. The effect of acoustic forcing on trailing edge separation and near wake development of an airfoil
5. The effect of sound on vortex shedding from cylinders
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