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Temperature measurement of cryogenic nitrogen jets at supercritical pressure
https://jaxa.repo.nii.ac.jp/records/39552
https://jaxa.repo.nii.ac.jp/records/39552658ea583-eb6c-4d1e-87c7-47fffca80a6e
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-09-24 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Temperature measurement of cryogenic nitrogen jets at supercritical pressure | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
著者 |
Tani, Hiroumi
× Tani, Hiroumi× Teramoto, S.× Toki, T.× Yoshida, S.× Yamaguchi, K.× Okamoto, K. |
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著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
出版者(英) | ||||||
出版者 | European Conference for Aeronautics and Space Sciences | |||||
書誌情報 | 発行日 2013-07 | |||||
関係URI | ||||||
識別子タイプ | URI | |||||
関連識別子 | https://eucass.eu/2013/index.html | |||||
関連名称 | https://eucass.eu/2013/index.html | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 5th European Conference for Aeronautics and Space Sciences, EUCASS 2013 (July 1-5, 2013.), Munich, Germany | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | "Many of liquid rocket engines used in first stage of launch vehicles operate at a pressure above the critical pressure of oxygen, 5.04 MPa. The cryogenic oxygen injected into a combustion chamber is heated up to several thousand kelvin, therefore the high-density cryogenic oxygen necessarily experiences sudden expansion called “pseudo-boiling”1 at the pseudo-critical temperature. The pseudo-boiling has large impact on the mixing characteristics, hence a jet injected from a temperature below the pseudo-critical temperature must be distinguished from that injected from a temperature above the pseudo-critical temperature. The former is referred to as “transcritical jet” while the latter is simply called supercritical jet. Quantitative measurement data of transcritical jets are indispensable both for the better understanding of mixing phenomena and for the validation of numerical methods, but there are only few quantitative experimental data made public.2 In this report, axial and radial temperature profiles of a single phase cryogenic nitrogen jet under supercritical pressure are measured, and the influence of pseudo-boiling upon the jet mixing will be discussed." | |||||
ISBN | ||||||
識別子タイプ | ISBN | |||||
関連識別子 | 978-84-941531-0-5 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1510093000 |