Incipient Separation for Hypersonic Shock Wave/Turbulent Boundary Layer Interaction
Shock/turbulent boundary layer interaction (STBLI) is a prevalent and complex flow phenomenon in the aerospace sector that significantly impacts the aerodynamic performance of vehicles. This study investigated the incipient separation conditions of a hypersonic oblique shock wave impinging on a turb...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | zho |
| Published: |
China Astronautic Publishing CO., LTD. ; Editorial Office of Physics of Gases
2025-05-01
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| Series: | 气体物理 |
| Subjects: | |
| Online Access: | http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.1149 |
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