Computational Investigation of Flow Control over Wings
Author:
Affiliation:
1. FORTH / IACM
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-477
Reference31 articles.
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2. Chandrasekhara, M. S., Wilder, M. C., and Carr, L. W. "Compressible Dynamic Stall Control: a Comparison of DifferentApproaches,"AIAA Paper99-3122,1999.
3. Forcing level effects of internal acoustic excitation on the improvement of airfoil performance
4. Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation
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