粗鲁的人
发表于 2025-3-26 23:38:22
Extension of Numerical Methods and Preliminary Control Assessment (Task 2) validated by the airfoil experiments of Task 3 and used for a preliminary assessment of the merits of passive shock control. A total of seven contributors have participated in the numerical studies, namely, . and the Universities of . and ..
Erythropoietin
发表于 2025-3-27 01:30:14
Introductiono study, numerically and experimentally, the effect of passive shock boundary layer interaction control (SBLIC) by ventilation on the design and off-design performance of primarily laminar-type airfoils and wings. The considerations leading to this research are outlined in what follows.
harangue
发表于 2025-3-27 06:05:23
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安定
发表于 2025-3-27 10:09:34
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menopause
发表于 2025-3-27 15:43:14
Overall Conclusion and Future Workement in the buffet boundary can be achieved. Also other configurations, such as engine inlets, where passive control may be of merit, have been identified The investigations have furthermore shed new light on the complex subject of shock wave boundary layer interaction and have highlighted new acti
欢乐东方
发表于 2025-3-27 20:38:41
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多嘴多舌
发表于 2025-3-28 01:01:57
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伸展
发表于 2025-3-28 04:37:05
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管理员
发表于 2025-3-28 06:28:04
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难解
发表于 2025-3-28 12:22:32
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