Sweep and compressibility effects on active separation control at high Reynolds numbers
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-410
Reference25 articles.
1. Delay of airfoil stall by periodic excitation
2. Oscillatory Control of Separation at High Reynolds Numbers
3. Seifert, A. and Pack, L.G. "Suppression of Shock-induced Separationby Oscillatory Excitation0022, (AIAA paper 99-0925), submittedtoJ.Aircraft, March 1999.
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