Mitigation of Dynamic Stall over a Pitching Finite Wing Using High-Frequency Actuation
Author:
Affiliation:
1. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058731
Reference29 articles.
1. Unsteady Airfoils
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4. The effect of a leading-edge slat on the dynamic stall of an oscillating airfoil
5. Unsteady Stall Control Using Dynamically Deforming Airfoils
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