Effect of Mach Number on Stability of Boundary Layer Over a Rotating Cone in Hypersonic Flow
Spinning vehicles achieve gyroscopic effects by rotating around their axis. However, transition significantly influences the stability of flight. In this work, a study of instability on the unstable modes in boundary layers over a rotating cone in hypersonic flows was presented with linear stability...
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| Autors principals: | , , , |
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| Format: | Artigo |
| Idioma: | Chinês |
| Publicat: |
China Astronautic Publishing CO., LTD. ; Editorial Office of Physics of Gases
2025-05-01
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| Col·lecció: | 气体物理 |
| Matèries: | |
| Accés en línia: | http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.1121 |
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