Oversee 发表于 2025-3-28 15:35:38

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nocturia 发表于 2025-3-28 22:32:32

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arousal 发表于 2025-3-28 23:02:41

NACA0012 with Aileron (Marianna Braza)ena arising as the result of the shock wave / boundary layer interaction in transonic flow over a NACA 0012 airfoil equipped with an aileron. The transonic buffet is a natural and self-sustaining oscillation of the shock wave and the separated flow region, caused by pressure fluctuation.

包庇 发表于 2025-3-29 03:49:03

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Memorial 发表于 2025-3-29 10:48:50

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guzzle 发表于 2025-3-29 12:23:14

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Conscientious 发表于 2025-3-29 15:59:12

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我还要背着他 发表于 2025-3-29 21:22:17

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macabre 发表于 2025-3-30 01:57:03

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手铐 发表于 2025-3-30 04:59:23

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查看完整版本: Titlebook: Unsteady Effects of Shock Wave induced Separation; Piotr Doerffer,Charles Hirsch,George N. Barakos Conference proceedings 20111st edition