COMPUTATIONAL AND EXPERIMENTAL STUDY OF SPANWISE SYNTHETIC JET FLOW CONTROL

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Computational and Experimental Study of Spanwise Synthetic Jet Flow Control.pdf (6.81 MB)

Date

2024-06-28

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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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Keywords

Airfoil, CFD, SJA

Citation

URI

https://hdl.handle.net/1807/142812

DOI

https://doi.org/10.48550/arXiv.2412.07726

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Attribution-ShareAlike 4.0 International

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http://creativecommons.org/licenses/by-sa/4.0/

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Department of Mechanical and Industrial Engineering
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