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

doi:10.1007/s12217-022-09991-y

	Simulation Analysis of Liquid Flow in a Vane-type Surface Tension Tank
	Wu, Zongyu 6; Li, Kai 4,5; Han, Wei 3; Li, Guangyu 2; Fan, Chengguang 6; Xu, Bingui 1
刊名	MICROGRAVITY SCIENCE AND TECHNOLOGY
	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
DOI	10.1007/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
内容类型	期刊论文
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,&Xu, Bingui.(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.