超臨界圧における液体水素の熱伝達特性(1)(直管における実験と既存整理式との比較)

Material type: 文書・図像類

Author: 新野, 正之ほか

Publisher: 航空宇宙技術研究所

Publication date: 1979-08

Material Format: Digital

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Note (General)：: The cooling problem in the thrust chamber is one of the most critical problems in the development of the rocket engine. Thus the engine system design ...

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Material Type: 文書・図像類
Title: 超臨界圧における液体水素の熱伝達特性(1)(直管における実験と既存整理式との比較)
Author/Editor: 新野, 正之
鈴木, 昭夫
熊川, 彰長
坂本, 博
佐々木, 正樹
NIINO, Masayuki
SUZUKI, Akio
KUMAKAWA, Akinaga
SAKAMOTO, Hiroshi
SASAKI, Masaki
Author Heading: 新野, 正之
鈴木, 昭夫
熊川, 彰長
坂本, 博
佐々木, 正樹
NIINO, Masayuki
SUZUKI, Akio
KUMAKAWA, Akinaga
SAKAMOTO, Hiroshi
SASAKI, Masaki
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1979-08
Publication Date (W3CDTF): 1979-08
Alternative Title: Heat Transfer Characteristics of Liquid Hydrogen at Super Critical Pressure (Heat Transfer Experimental Data and Comparisons with Previous Correlations)
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-583
No. or year of volume/issue: 583
Volume: 583
Pages: 17-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): The cooling problem in the thrust chamber is one of the most critical problems in the development of the rocket engine. Thus the engine system design is often greatly influenced by the decision of what kind of cooling system to adopt. The nondimentional design equations, which were previously proposed by many investigators, however, are very different from each other. Consequently we can not decide what is the best adequate equation for the design. Such being the case, the authors have begun investigation of the heat transfer characteristics of liquid hydrogen in relation to the design of engines being developed in Japan. The authors consider the main causes of the disagreement between many correlation equations to be as follws. (1)Many investigators did not distinguish among the differences of heat transfer phenomena found near the pseudo critical temperature T*cr. (2)The investigators did not pay enough attentions to the surface roughness of the test tubes and the complicated behavior of the entrance effects. Thus the present report intends to compare the author’s experimental data with these previously correlated equations from these two points of view.
資料番号: NALTR0583000
レポート番号: NAL TR-583
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44837&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44837&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ