Control of laminar separation over airfoils by acoustic excitation
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-565
Reference15 articles.
1. Separation by Sound," AIAA Paper 84-2298, Oct. 1984, 5. Laman, K.B.M.Q., Bar-Sever, A, and Mangalam,
2. Effect of acoustic excitation on the flow over a low- Re airfoil
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1. Separation Control by External Acoustic Excitation at Low Reynolds Numbers;AIAA Journal;2013-06
2. Active Flow Control Strategy of Laminar Separation Bubbles Developed over Subsonic Airfoils at Low Reynolds Numbers;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
3. Control of flow separation using adaptive airfoils;35th Aerospace Sciences Meeting and Exhibit;1997-01-06
4. Status and outlook of flow separation control;29th Aerospace Sciences Meeting;1991-01-07
5. A natural low-frequency oscillation of the flow over an airfoil near stalling conditions;Journal of Fluid Mechanics;1989-05
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