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火箭推进剂液体晃动关机响应的数值仿真

Numerical simulation of slosh of the propellant fuel during the period of shut-down of the rocket

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【作者】 包光伟王振强张天翔陈健

【Author】 BAO Guang wei 1,WANG Zhen qiang 1,ZHANG Tian xiang 2,CHEN Jian 2 (1 Department of Engineering Mechanics,Shanghai Jiao Tong University,Shanghai 200030; 2 No.805 Research Institute,Shanghai Academy of Spaceflight Technology,Shanghai 201108)

【机构】 上海交通大学工程力学系上海航天技术研究院第805研究所上海航天技术研究院第805研究所 上海200030上海200030

【摘要】 本文采用 VOF方法对火箭发动机关机阶段所引起的液体晃动进行了数值仿真 ,以氧化剂贮箱为例 ,得到了贮箱无阻尼环和带阻尼环时的晃动仿真图和液体质心变化曲线。检验了 VOF方法处理碎波的能力。

【Abstract】 In the present paper,the Volume Of Fluid(VOF) method is employed to simulate the slosh of liquid in container during the period of shut down of the rocket numerically.As an example,the slosh of the oxidizer has been simulated and a series of the simulation figures have been plotted in both cases of the container with/without damping ring.The investigation shows that VOF method has a powerful capability even to deal with the problem as the free surface breaking up.

【关键词】 液体晃动VOF方法航天器动力学
【Key words】 Liquid sloshVOF methodDynamics of spacecraft
  • 【文献出处】 宇航学报 ,Journal of Astronautics , 编辑部邮箱 ,2002年02期
  • 【分类号】V421.4
  • 【被引频次】32
  • 【下载频次】241
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