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Simulation Analysis of Liquid Flow in a Vane-type Surface Tension Tank

文献类型：期刊论文

作者Wu, Zongyu6; Li, Kai4,5; Han, Wei3; Li, Guangyu2; Fan, Chengguang6; Xu, Bingui1; Li K(李凯)
刊名MICROGRAVITY SCIENCE AND TECHNOLOGY
出版日期2022-08-18
卷号34期号:5页码:8
关键词Simulation analysis Surface tension tank T-shaped vane Perforated vane
ISSN号0938-0108
DOI10.1007/s12217-022-09991-y
通讯作者Li, Kai(likai@imech.ac.cn) ; Han, Wei(hanwei1984@hotmail.com)
英文摘要With the development of space technology, space missions are becoming more and more complex, which puts forward higher requirements for the service life and anti-interference ability of fuel tanks. Due to its lightweight, long service life, and easy processing, the vane-type surface tension tank has been more and more widely used. The vane-type tank enables propellant management with surface tension, however the surface tension is weak. As a result, the control ability of the propellant is limited, which is not suitable for high dynamic maneuvering conditions. This problem limits the development of the vane-type tank and the expansion of mission scenarios. In order to further enhance the propellant management ability of the vane-type surface tension tank, this paper numerically investigated the influence of the T-shaped vane and the perforated vane on propellant management. By applying different boundary conditions, its liquid control ability under complex working conditions is checked. The results show that the T-shaped vane can obviously enhance the liquid transport ability of the tank; the perforated vane can significantly reduce weight, however it weakens the liquid transport ability. The work of this paper can be used to guide the design of the vane-type surface tension tank and has certain guiding significance for the improvement of propellant management performance.
资助项目National Natural Science Foundation of China[52105290] ; National Natural Science Foundation of China[12172363] ; Key Research Program of Frontier Sciences, CAS[QYZDY-SSW-JSC040]
WOS研究方向Engineering ; Thermodynamics ; Mechanics
语种英语
WOS记录号WOS:000841760500002
资助机构National Natural Science Foundation of China ; Key Research Program of Frontier Sciences, CAS
源URL[http://dspace.imech.ac.cn/handle/311007/89907]  
专题力学研究所_国家微重力实验室
通讯作者Li, Kai; Han, Wei
作者单位1.Shandong Inst Space Elect Technol, Yantai 264003, Shandong, Peoples R China
2.Nanchang Hangkong Univ, Sch Aircraft Engn, Nanchang 330063, Jiangxi, Peoples R China
3.Chinese Acad Mil Sci, Natl Innovat Inst Def Technol, Beijing 100000, Peoples R China
4.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China
5.Chinese Acad Sci, Inst Mech, Key Lab Micrograv, Natl Micrograv Lab, Beijing 100190, Peoples R China
6.Natl Univ Def Technol, Coll Aerosp Sci & Engn, Deya Rd 109, Changsha 410073, Hunan, Peoples R China
推荐引用方式
GB/T 7714		 Wu, Zongyu,Li, Kai,Han, Wei,et al. Simulation Analysis of Liquid Flow in a Vane-type Surface Tension Tank[J]. MICROGRAVITY SCIENCE AND TECHNOLOGY,2022,34(5):8.
APA Wu, Zongyu.,Li, Kai.,Han, Wei.,Li, Guangyu.,Fan, Chengguang.,...&李凯.(2022).Simulation Analysis of Liquid Flow in a Vane-type Surface Tension Tank.MICROGRAVITY SCIENCE AND TECHNOLOGY,34(5),8.
MLA Wu, Zongyu,et al."Simulation Analysis of Liquid Flow in a Vane-type Surface Tension Tank".MICROGRAVITY SCIENCE AND TECHNOLOGY 34.5(2022):8.

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来源：力学研究所

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