Effect of leading-edge tubercles on the flow over low-aspect-ratio wings at low Reynolds number

Theoretical and Applied Mechanics Letters - Tập 13 - Trang 100386 - 2023
Pengxin Yang1, Yichen Zhu1, Jinjun Wang1
1Institute of Fluid Mechanics, Beijing University of Aeronautics and Astronautics, Beijing, 100191, China

Tài liệu tham khảo

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