COMPUTATIONAL AND EXPERIMENTAL STUDY OF SPANWISE SYNTHETIC JET FLOW CONTROL
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Abstract
This study investigates the reattachment of flow on a stalled NACA 0025 airfoil with an array of circular synthetic jet actuators. Experimental flow visualizations are used to assess the spanwise control authority of the array and the three-dimensionality of the flow. Numerical simulations provide insights into the flow structures created by the actuation, and how they evolve with different parameters.
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Airfoil, CFD, SJA
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https://doi.org/10.48550/arXiv.2412.07726
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