| 摘要: |
| 针对多级导弹级间热分离这一复杂环境条件，用数值模拟的方法对级间段流场进行了预示。计算采用Ｇｏｄｕｎｏｖ有限体积格式，对非定常轴对称欧拉方程进行求解。计算结果为级间分离段和发动机热防护的设计提供了理论依据。 |
| 关键词: 多级导弹 级间分离 数值仿真 有限体积法 |
| DOI： |
| 分类号:V430 |
| 基金项目: |
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| NUMERICAL SIMULATION OF FLOW FIELD FOR THERMAL SEPARATION OF MULTISTAGE MISSILE |
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Li Jiang, Xiao Yumin, Sun Dechuan, Cai Timin
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Coll of Astronautics,Northwestern Polytechnical Univ ,Xi′an,710072
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| Abstract: |
| The thermal stage separation condition of multi stage missile is very complex.The flow field for thermal stage separation part is predicted with numerical simulation in this paper.The Godunov finite volume method is used to solve the unsteady axisymmetric Eluer equations.The results can provide basis for the design of the thermal protection of motor case the stage separation part |
| Key words: Multi-stage missile Stage separation Numerical simulation Finite volume method |
