Active control of separated flows on generic configurations 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/10.2514/6.1999-3403
Reference36 articles.
1. Stratford, B. S., n Experimental Flow with Zero Skin-Friction Throughout its Region of Pressure Rise" Journal of Fluid MechanicsVol.5, pp.17-35, 1959.
2. An approach to turbulent incompressible separation under adverse pressure gradients
3. Liebeck, R. H. "Optimization of Airfoils for Maximum Lift0022, PhD Thesis,University of Illinois, 1968.
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