摘要: An experimental investigation on Shockwave/Boundary Layer Interaction (SBLI) induced by an unswept fin is performed at Mach 5 with both laminar and transitional boundary layers. The unswept fin geometry is the scaled-down model (3... 展开
作者 | Sathyan Padmanabhan Lucas Jouannais James A. S. Threadgill Jesse C. Little | ||
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作者单位 | |||
文集名称 | Fluid Dynamics | ||
出版年 | 2023 | ||
会议名称 | AIAA SciTech Forum and Exposition | ||
卷/页码 | vol. 4 / 2556-2571 | 开始页/总页数 | 00002556 / 16 |
会议地点 | Maryland(US) | 会议年 | 2023 |
馆藏号 | P2400039 |