高文, 林博颖, 吴东亮, 等. 基于滑移流模型的真空容器内羽流流场数值仿真[J]. 航天器环境工程, 2024, 41(2): 129-137 DOI: 10.12126/see.2023151
引用本文: 高文, 林博颖, 吴东亮, 等. 基于滑移流模型的真空容器内羽流流场数值仿真[J]. 航天器环境工程, 2024, 41(2): 129-137 DOI: 10.12126/see.2023151
GAO W, LIN B Y, WU D L, et al. Numerical simulation of plume flow field in vacuum chamber based on slip flow model[J]. Spacecraft Environment Engineering, 2024, 41(2): 129-137 DOI: 10.12126/see.2023151
Citation: GAO W, LIN B Y, WU D L, et al. Numerical simulation of plume flow field in vacuum chamber based on slip flow model[J]. Spacecraft Environment Engineering, 2024, 41(2): 129-137 DOI: 10.12126/see.2023151

基于滑移流模型的真空容器内羽流流场数值仿真

Numerical simulation of plume flow field in vacuum chamber based on slip flow model

  • 摘要: 预示真空容器内羽流的力、热分布规律是制定大型真空羽流试验方案、提升试验环境模拟有效性的关键前提之一。针对“嫦娥七号”飞跃器点火试验,利用考虑H2O与CO2吸附的滑移流计算流体力学(CFD)方法,对真空容器内羽流流场压力、温度及气体组分时空分布的初期变化进行了仿真计算。结果表明,流场整体温度与H2O组分质量分数均随时间推移呈急剧上升后平稳下降趋势,而压力则随时间推移呈波动上升趋势。基于该结论提出了试验优化建议。该方法为真空容器内羽流流场仿真提供了新思路,可为后续相关试验方案设计提供支撑。

     

    Abstract: Predicting the aerodynamic and thermal distributions of the plume in vacuum chamber is one of the key prerequisites for developing a large-scale vacuum plume test scheme and improving the simulation effectiveness of the experimental environment. For the ignition test of China's Chang’e-7 leaper, a slip flow computational fluid dynamics (CFD) method taking the adsorption of H2O and CO2 into consideration was used to simulate the initial changes in the spatial-temporal distributions of pressure, temperature and gas composition of the plume flow field in a vacuum chamber. The results indicate that both the temperature and mass fraction of H2O component in the flow field increase rapidly and then decrease smoothly, while the pressure fluctuates upward over time. Based on this conclusion, experimental optimization suggestions are proposed. The method provides a new approach for simulating the plume flow field in vacuum chamber, which may support for the subsequent design of relevant test schemes.

     

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