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Free shear layers with Kelvin-Helmholtz instability are present in many applications, including flow separation over an airfoil. This work is on the excitation of K-H instability using plasma actuators to control the flow.
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This page is a summary of: Flow Separation Control over a Thin Post-Stall Airfoil: Effects of Excitation Frequency, AIAA Journal, January 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j057796.
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