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

doi:10.1007/s12217-022-09991-y

IMECH-IR > 微重力重点实验室

	Simulation Analysis of Liquid Flow in a Vane-type Surface Tension Tank
	Wu, Zongyu 1; Li K(李凯)2,3 ; Han, Wei 4; Li, Guangyu 5; Fan, Chengguang 1; Xu, Bingui 6
通讯作者	Li, Kai(likai@imech.ac.cn) ; Han, Wei(hanwei1984@hotmail.com)
发表期刊	MICROGRAVITY SCIENCE AND TECHNOLOGY
	2022-08-18
卷号	34 期号:5 页码:8
ISSN	0938-0108
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.
关键词	Simulation analysis Surface tension tank T-shaped vane Perforated vane
DOI	10.1007/s12217-022-09991-y
收录类别	SCI ; EI
语种	英语
WOS记录号	WOS:000841760500002
WOS研究方向	Engineering ; Thermodynamics ; Mechanics
WOS类目	Engineering, Aerospace ; Thermodynamics ; Mechanics
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]
项目资助者	National Natural Science Foundation of China ; Key Research Program of Frontier Sciences, CAS
论文分区	二类
力学所作者排名	1
RpAuthor	Li, Kai ; Han, Wei
引用统计	被引频次：1[WOS] [WOS记录] [WOS相关记录]
文献类型	期刊论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/89908
专题	微重力重点实验室
作者单位	1.Natl Univ Def Technol, Coll Aerosp Sci & Engn, Deya Rd 109, Changsha 410073, Hunan, Peoples R China; 2.Chinese Acad Sci, Inst Mech, Key Lab Micrograv, Natl Micrograv Lab, Beijing 100190, Peoples R China; 3.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China; 4.Chinese Acad Mil Sci, Natl Innovat Inst Def Technol, Beijing 100000, Peoples R China; 5.Nanchang Hangkong Univ, Sch Aircraft Engn, Nanchang 330063, Jiangxi, Peoples R China; 6.Shandong Inst Space Elect Technol, Yantai 264003, Shandong, Peoples R China
推荐引用方式 GB/T 7714	Wu, Zongyu,Li K,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,李凯,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.

条目包含的文件		下载所有文件
文件名称/大小	文献类型	版本类型	开放类型	使用许可
Jp2022FA207_2022_Sim（1345KB）	期刊论文	出版稿	开放获取	CC BY-NC-SA	浏览下载