Numerical Simulation of the Transient Flow Field Induced by the Sub-booster Releasing from the Missile Body
碩士 === 中正理工學院 === 兵器系統工程研究所 === 88 === The flow field induced by the separation of a strap-on booster during the flight of strap-on launch vehicles is highly complex and inherently unsteady. Most previous studies on these flow fields were focused on experimental works. However, the expe...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2000
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| Online Access: | http://ndltd.ncl.edu.tw/handle/33297641268579218308 |