Use of Piezoelectric Actuators for Airfoil Separation Control
Author:
Affiliation:
1. Tel-Aviv University, Tel-Aviv 69978, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.549
Reference4 articles.
1. Delay of airfoil stall by periodic excitation
2. Oscillatory control of separation and high Reynolds numbers
3. Rae, W. H., Jr., and Pope, A., Low Speed Wind Tunnel Testing, 2nd ed.Wiley, New York, 1984, pp.349-361.
4. Exploratory study of vortex-generating devices for turbulent flow separation control
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