Poststall Behavior of a Wing Under Externally Imposed Sound
Author:
Affiliation:
1. University of New South Wales, Sydney, New South Wales 2052, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2861
Reference11 articles.
1. Development of advanced circulation control wing high-lift airfoils
2. Schlichting, H., Boundary Layer Theory, 7th ed.McGraw-Hill, New York, 1987, pp.378-382.
3. Effects of freestream disturbances on boundary-layer transition.
4. Control of flow separation by sound
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