Simulation analysis of liquid sloshing separation in spacecraft with tank based on SPH method

被引：0
|
作者：
Liu, Hanwu [1 ,2 ,3 ]
Zhang, Hua [1 ,2 ,3 ]
Hu, Zhenyu [1 ,3 ]
Wang, Jintong [1 ]
Yu, Zhi [1 ]
Yuan, Yong [1 ]
机构：
[1] Aerospace Systems Engineering Shanghai, Shanghai,201109, China
[2] Shanghai Key Laboratory of Spacecraft Mechanism, Shanghai,201108, China
[3] Joint Laboratory of Planetary Terramechanics and Bionic Engineering, Shanghai,201109, China
来源：
Zhongguo Kexue Jishu Kexue/Scientia Sinica Technologica | 2021年 / 51卷 / 08期
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页码：938 / 947
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