| Simulation Analysis of Liquid Flow in a Vane-type Surface Tension Tank | |
Wu, Zongyu1; Li K(李凯)2,3 ; Han, Wei4; Li, Guangyu5; Fan, Chengguang1; Xu, Bingui6
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| Corresponding Author | Li, Kai([email protected]) ; Han, Wei([email protected]) |
| Source Publication | MICROGRAVITY SCIENCE AND TECHNOLOGY
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| 2022-08-18 | |
| Volume | 34Issue:5Pages:8 |
| ISSN | 0938-0108 |
| Abstract | 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. |
| Keyword | Simulation analysis Surface tension tank T-shaped vane Perforated vane |
| DOI | 10.1007/s12217-022-09991-y |
| Indexed By | SCI ; EI |
| Language | 英语 |
| WOS ID | WOS:000841760500002 |
| WOS Research Area | Engineering ; Thermodynamics ; Mechanics |
| WOS Subject | Engineering, Aerospace ; Thermodynamics ; Mechanics |
| Funding Project | National Natural Science Foundation of China[52105290] ; National Natural Science Foundation of China[12172363] ; Key Research Program of Frontier Sciences, CAS[QYZDY-SSW-JSC040] |
| Funding Organization | National Natural Science Foundation of China ; Key Research Program of Frontier Sciences, CAS |
| Classification | 二类 |
| Ranking | 1 |
| Contributor | Li, Kai ; Han, Wei |
| Citation statistics | |
| Document Type | 期刊论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/89908 |
| Collection | 微重力重点实验室 |
| Affiliation | 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 |
| Recommended Citation 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.Rp_Au:Li, Kai, Han, Wei |
| 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. |
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| Jp2022FA207_2022_Sim（1345KB） | 期刊论文 | 出版稿 | 开放获取 | CC BY-NC-SA | View Download | |
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