Analysis of Influencing Factors of Boundary Layer Transition During Ascent Phase of Hypersonic Vehicle
The transition of the boundary layer is an important issue that must be considered in the design of hypersonic vehicles. During the ascent phase of the vehicle, both the Mach number and the flight altitude increase simultaneously and affect the location of transition jointly. This paper investigated...
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| Principais autores: | , , |
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| Format: | Artigo |
| Jezik: | Chinês |
| Izdano: |
China Astronautic Publishing CO., LTD. ; Editorial Office of Physics of Gases
2024-11-01
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| Serija: | 气体物理 |
| Teme: | |
| Online dostop: | http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.1115 |
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