Equivalent Test Method Using Detonation Shock Tubes for Unsteady Flows During Rocket Interstage Separation
Utilizing detonation shock tubes to evaluate the rocket interstage separation process holds broad application prospects. The article first established an equivalent simulation model for the average pressure change within the interstage section during the interstage pressure build-up phase through th...
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| Main Authors: | , , , , , |
|---|---|
| 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.2096-1642.1130 |
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