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低温贮箱在轨压增数值研究

Numerical simulation of pressurization process in liquid hydrogen tank in-orbit

中文摘要英文摘要

本文首先采用基于VOF模型的CFD方法获得微重力下气液界面的分布特征,然后采用Lump-Vapor模型对液氢贮箱的气相区和液相区分别求解,并采用UDF用户程序考虑气液相变热质交换,从而实现了对液氢贮箱压增过程的快速预测。模拟结果表明,在微重力下,表面张力作用凸现,气液界面形状在7200s后基本达到稳定。对于本文计算工况,在6.5W/m2的空间漏热热流下,经过4天的在轨运行,气液相界面温升约4.87K;压增速率约为70.75kPa/天。在保证一定精度的前提下,采用Lump-Vapor模型不仅较好地预测了箱体压增特性和物理场分布规律,而且还显著提高了运行效率,节省大量计算时间。

nterface distribution in microgravity could be easily obtained based on VOF model of CFD. And ullage zone and liquid zone of hydrogen tank were computing separately with Lump-Vapor model. With the UDF considering the heat and mass transfer happened in gas-liquid interface, pressurization process of hydrogen tank could be predicted quickly. The simulation results indicted that the gas-liquid interface shape achieved stability in 7200 seconds under the cooperation of microgravity and surface tension. After 4 days in orbit, the temperature of interface increased 4.87K, and the pressurization rate was about 70.75kPa per day with the constant space heat leakage flux of 6.5W/m2. In the premise of certain precision, the Lump-Vapor model can not only better predict the tank pressure characteristics and physical distribution, but also safe more computing time, significantly improve operation efficiency.

赵志翔、王磊、晋永华、刘展、厉彦忠

航空航天技术力学工程基础科学

体火箭增压过程低温液氢贮箱Lump-Vapor模型数值模拟

liquid rocketpressurization processLump-Vapor modelcryogenic hydrogen tanknumerical simulation

赵志翔,王磊,晋永华,刘展,厉彦忠.低温贮箱在轨压增数值研究[EB/OL].(2013-12-06)[2025-08-16].http://www.paper.edu.cn/releasepaper/content/201312-116.点此复制

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