Numerical Simulation of the Effect of Swing Center on a Supersonic Split Line Nozzle
A numerical investigation was performed in the present work to uncover the effect of swing center on a supersonic split line nozzle. Detailed nozzle internal flow and thrust performance were analysed, for serval swing center positions. It is found that, the step formed by the nozzle swing causes a b...
Saved in:
| Main Authors: | , , , , , |
|---|---|
| Format: | Article |
| Language: | zho |
| Published: |
China Astronautic Publishing CO., LTD. ; Editorial Office of Physics of Gases
2025-07-01
|
| Series: | 气体物理 |
| Subjects: | |
| Online Access: | http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.1134 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|