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Flow field control over a high-aspect-ratio wing using a plasma actuator at low Reynolds number
Zhiming MA, Xin ZHANG
Acta Aeronautica et Astronautica Sinica . 2026, (5): 132359 -132359 .  DOI: 10.7527/S1000-6893.2025.32359

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341