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...
Saved in:
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | zho |
| Published: |
China Astronautic Publishing CO., LTD. ; Editorial Office of Physics of Gases
2025-05-01
|
| Series: | 气体物理 |
| Subjects: | |
| Online Access: | http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.1121 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|