摘要: Three different sub-grid scale large eddy simulations (LES) were assessed for shock wave turbulent boundary layer interaction (STBLI) of hypersonic flow over hollow cylinder flare with Ansys Fluent. The incoming flow is at Mach 6 ... 展开
作者 | Sogol Pirbastami Darrell Pepper | ||
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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. 2 / 956-969 | 开始页/总页数 | 00000956 / 14 |
会议地点 | Maryland(US) | 会议年 | 2023 |
馆藏号 | P2400037 |