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Optimization of the Experimental Set-up for a Turbulent Separated Shear Flow Control by Plasma Actuator Using Genetic Algorithms

Advances in Effective Flow Separation Control for Aircraft Drag Reduction Pub Date : 2019-10-18 DOI:10.1007/978-3-030-29688-9_9
N. Benard, J. Pons-Prats, J. Périaux, J. Bonnet, G. Bugeda
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用遗传算法优化等离子体作动器控制湍流分离剪切流的实验装置
本文章由计算机程序翻译，如有差异，请以英文原文为准。
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Advances in Effective Flow Separation Control for Aircraft Drag Reduction
Advances in Effective Flow Separation Control for Aircraft Drag Reduction
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