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arXiv · 2412.07726

Computational And Experimental Study of Spanwise Synthetic Jet Flow Control

Howard Ho·Adnan Machado·Pierre Sullivan
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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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Howard Ho, Adnan Machado, Pierre Sullivan. 2024-12-10. Computational And Experimental Study of Spanwise Synthetic Jet Flow Control. https://arxiv.org/abs/2412.07726

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