Item type |
紀要論文 / Departmental Bulletin Paper(1) |
公開日 |
2015-03-26 |
タイトル |
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タイトル |
Dynamic Heat Transfer Mechanism of Two-phase Closed Thermosyphon |
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言語 |
en |
言語 |
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言語 |
eng |
資源タイプ |
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資源タイプ識別子 |
http://purl.org/coar/resource_type/c_6501 |
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資源タイプ |
departmental bulletin paper |
著者 |
NEGISHI, Kanji
KANEKO, Ken-ichi
KUSUMOTO, Fusao
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著者所属(英) |
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en |
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Department of Aeronautical Engineering, College of Engineering, University of Osaka Prefecture |
著者所属(英) |
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en |
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Department of Aeronautical Engineering, College of Engineering, University of Osaka Prefecture |
著者所属(英) |
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en |
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Department of Aeronautical Engineering, College of Engineering, University of Osaka Prefecture |
出版者 |
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出版者 |
宇宙科学研究所 |
出版者(英) |
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出版者 |
Institute of Space and Astronautical Science |
書誌情報 |
en : The Institute of Space and Astronautical Science report. S.P. : Proceedings of the Symposium on Mechanics for Space Flight 1985
巻 4,
p. 143-151,
発行日 1986-03
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抄録(英) |
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内容記述タイプ |
Other |
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内容記述 |
The heat transfer mechanism of a two-phase closed thermosyphon has been dynamically analysed in the periodically motive behavior of working fluid with boiling. It is important problem in order to obtain high heat transfer performance how the liquid film of the working fluid can be held for longer time on the wider area of the evaporator heating wall and how the active evaporation can be kept there. |
ISSN |
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収録物識別子タイプ |
ISSN |
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収録物識別子 |
0288-433X |
書誌レコードID |
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収録物識別子タイプ |
NCID |
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収録物識別子 |
AA10455137 |
資料番号 |
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内容記述タイプ |
Other |
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内容記述 |
資料番号: SA0033541000 |