POD Based Separation Control on the NACA0015 Airfoil
Author:
Affiliation:
1. US Air Force Academy
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-297
Reference19 articles.
1. The control of flow separation by periodic excitation
2. Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation
3. Delay of airfoil stall by periodic excitation
4. Donovan, J.F.,Kral,L.D., Cary, A.W., 1998, Active Flow Control appliedtoanAirfoil,AIAA 98-0210
5. Seifert, A., Pack, L.G., 2003, Compressibility and Excitation Location Effects on High Reynolds Numbers Active Separation Control,Journal of Aircraft, Vol.40,No. 1, pp.110-119.
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