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We propose a framework to reduce airfoil drag from dynamic stall. The approach employs computationally inexpensive, physics-based methods which are used to inform the position and finite duty cycle of flow actuation. The framework is assessed by testing the actuation in a high-fidelity numerical simulation environment. The physical mechanisms are then elucidated.

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This page is a summary of: Control of Deep Dynamic Stall by Duty-Cycle Actuation Informed by Stability Analysis, AIAA Journal, July 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j064980.
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