2011 Fiscal Year Final Research Report
Experimental and Numerical Research on Heat Transfer and Phase Change in Propellant Tanks of Space Vehicles
| Project/Area Number |
21686080
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| Research Category |
Grant-in-Aid for Young Scientists (A)
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| Allocation Type | Single-year Grants |
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| Research Field |
Aerospace engineering
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| Research Institution | The University of Tokyo |
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Principal Investigator |
HIMENO Takehiro 東京大学, 大学院・工学系研究科, 准教授 (60376506)
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| Project Period (FY) |
2009 – 2011
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| Keywords | 推進 / エンジン / 液体ロケット / 極低温 / 相変化 / 計算力学 |
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| Research Abstract |
For the prediction of heat transfer coupled with sloshing phenomena in the propellant tanks of reusable launch vehicle, the pressure drop induced by heat transfer and the dynamic motion of liquid in sub-scale vessels were experimentally observed and numerically investigated. The correlation between the pressure drop and liquid motion was confirmed in the experiment. The mechanisms enhancing heat transfer were discussed based on the computation. It was suggested that splash and wavy surface induced by violent motion of liquid cause the pressure drop in the closed vessel. In addition, as the preliminary investigation, non-isothermal sloshing of liquid nitrogen and liquid hydrogen were successfully visualized and pressure drop depending on the gaseous species was discussed.
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[Presentation] 基幹ロケット推進系開発計画2011
Author(s)
杵淵紀世志,東伸幸,更江渉,沖田耕一,谷直樹,小林弘明,八木下剛,北山治,姫野武洋
Organizer
1S13日本航空宇宙学会第55回宇宙科学技術連合講演会
Place of Presentation
松山
Year and Date
20110909-11
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[Presentation] Heat Exchange and Pressure Drop Enhanced by Sloshing2011
Author(s)
T. Himeno, D. Sugimori, K. Ishikawa, Y. Umemura, S. Uzawa, C. Inoue, T. Watanabe, S. Nonaka, Y. Naruo, Y. Inatani, K. Kinefichi, R. Yamashiro, T. Morito and K. Okita
Organizer
The 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Place of Presentation
San Diego
Year and Date
20110801-04
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