Effect of Acoustic Excitation Amplitude on Airfoil Boundary Layer and Wake Development
Author:
Affiliation:
1. University of Waterloo, Waterloo, Ontario N2L 3G1, Canada
2. University of Toronto, Toronto, Ontario M5S 3G8, Canada
3. Ryerson University, Toronto, Ontario M5B 2K3, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.25439
Reference22 articles.
1. The control of flow separation by periodic excitation
2. Influence of Sound upon Separated Flow over Wings
3. Effect of acoustic excitation on stalled flows over an airfoil
4. Control of flow separation by acoustic excitation
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