Active Control of Flow Separation from Supercritical Airfoil Leading-Edge Flap Shoulder
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
2. Tel-Aviv University, 69978 Ramat-Aviv, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.10294
Reference16 articles.
1. Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation
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3. Parametric Investigation of a High-Lift Airfoil at High Reynolds Numbers
4. 5Barlow, J. B., Rae, W. H., Jr., and Pope, A., Low Speed Wind Tunnel Testing, 3rd ed.Wiley, New York, 1999, pp.328-366.
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