書誌事項
- タイトル別名
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- Study of Composite Wick Heat Pipe
- フクゴウ ウィック ヒート パイプ ノ ケンキュウ
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説明
This paper describes the performance of the composite wick heat pipe, which has two kinds of wicks, namely, circumferential grooves as a pumping wick and sintered stainless metal felt as a transport wick.<BR>The maximum heat transfer rate and evaporator heat transfer coefficient was obtained by changing the influential parameters; groove geometry, porosity of felt, evaporator length and inclination angle. And a theoretical model has been developed to predict the maximum heat transfer rate of this type of the composite wick heat pipe. In this model, a liquid recession into the bottom of the groove due to the increased heat transfer rate, so called "LEVERETT effect, " was taken into consideration.<BR>It is concluded that the predicted maximum heat transfer rate agrees well with the experimental data.
収録刊行物
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- 日本航空宇宙学会誌
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日本航空宇宙学会誌 30 (339), 198-207, 1982
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282679483268352
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- NII論文ID
- 130003958478
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- NII書誌ID
- AN00189072
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- ISSN
- 24241369
- 00214663
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- NDL書誌ID
- 2448696
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可