Simulation Study on Outflow Characteristics of Cryogenic Propellant during Rocket Ascent
At the rocket launching stage, it is very important to supply sufficient and vapor-free liquid propellant to maintain the functioning of the main engine. Considering the working characteristics and design requirements of the outflow device of the cryogenic propellant tank, a computational fluid dyna...
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| Main Authors: | , , , , |
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| Format: | Article |
| Language: | zho |
| Published: |
Journal of Refrigeration Magazines Agency Co., Ltd.
2020-01-01
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| Series: | Zhileng xuebao |
| Subjects: | |
| Online Access: | http://www.zhilengxuebao.com/thesisDetails#10.3969/j.issn.0253-4339.2020.04.136 |
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