Wind Tunnel Tests and Modeling Analysis of Dynamic Boundary Layer Transition on a Blunt Cone with Continuously Increasing Reynolds Number
The region of boundary layer transition on a blunt cone alternates periodically with pitching motion, and simultaneously develops from end to forward due to increasing Reynolds number during flight. This dynamic process may induce instability of pitching motion. Based on the dynamic boundary layer t...
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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
2025-07-01
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| Series: | 气体物理 |
| Subjects: | |
| Online Access: | http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.1124 |
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