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ロケットエンジン燃焼室の入口近傍を想定した酸水素界面の微視的研究
https://jaxa.repo.nii.ac.jp/records/16186
https://jaxa.repo.nii.ac.jp/records/16186dd046eaa-c6f5-41ea-ad9d-937f22e84f53
名前 / ファイル | ライセンス | アクション |
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61856050.pdf (432.9 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ロケットエンジン燃焼室の入口近傍を想定した酸水素界面の微視的研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Molecular Dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Interfacial Properties | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Oxygen | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Hydrogen | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Microscopic study of oxygen-hydrogen interface around the inlet of rocket engine combustion chamber | |||||
著者 |
井川, 祥平
× 井川, 祥平× 津田, 伸一× Ikawa, Shohei× Tsuda, Shinichi |
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著者所属 | ||||||
信州大学 | ||||||
著者所属 | ||||||
信州大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Shinshu University | ||||||
著者所属(英) | ||||||
en | ||||||
Shinshu University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | |||||
書誌情報 |
平成24年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium: FY2012 発行日 2013-01 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県 | |||||
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 | Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Understanding of atomization properties of oxygen in coaxial jet flow around the inlet of rocket engine combustion chamber is important for CFD simulation with high fidelity. However, there is no experimental data of interfacial tension that influences the atomization properties. In this study, we conducted a Molecular Dynamics (MD) simulation for reproduction of oxygen-hydrogen interface in rocket engine combustion chamber, and then we studied the interfacial tension between liquid oxygen and gas hydrogen focusing microscopic structure of the interface. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: PDF | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: PDF | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0061856050 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: STCP-2012-050 |