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ヒドラジン/二酸化窒素同軸噴流の特異な二重火炎構造
https://jaxa.repo.nii.ac.jp/records/3849
https://jaxa.repo.nii.ac.jp/records/38491eb40681-15ca-4b82-b74d-e66570781374
名前 / ファイル | ライセンス | アクション |
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AA1530023014.pdf (3.0 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-04-28 | |||||
タイトル | ||||||
タイトル | ヒドラジン/二酸化窒素同軸噴流の特異な二重火炎構造 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | Double flame structure of hydrazine/nitrogen dioxide coaxial jets | |||||
著者 |
谷, 洋海
× 谷, 洋海× 寺島, 洋史× 越, 光男× 大門, 優× Tani, Hiroumi× Terashima, Hiroshi× Koshi, Mituo× Daimon, Yu |
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著者所属 | ||||||
宇宙航空研究開発機構情報・計算工学センター(JAXA)(JEDI) | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
横浜国立大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構情報・計算工学センター(JAXA)(JEDI) | ||||||
著者所属(英) | ||||||
en | ||||||
JAXA's Engineering Digital Innovation Center, Japan Aerospace Exploration Agency (JAXA)(JEDI) | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Yokohama National University | ||||||
著者所属(英) | ||||||
en | ||||||
JAXA's Engineering Digital Innovation Center, Japan Aerospace Exploration Agency (JAXA)(JEDI) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium 巻 JAXA-SP-14-010, p. 75-80, 発行日 2015-03-25 |
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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 | 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム (2014年7月3日-4日. 弘前文化センター), 弘前市, 青森県 | |||||
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 | 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium (July 3-4, 2014. Hirosaki Bunka Center), Hirosaki, Aomori, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Hydrazine (N2H4) nitrogen dioxide (NO2) co-flowing plane jets were simulated to explore the flame structures in hypergolic N2H4 nitrogen tetroxide (N2O4) bipropellant thrusters. The Navier-Stokes equations with a detailed chemical kinetics mechanism were solved in a manner of direct numerical simulation to reveal the interaction between fluid dynamics and the distinct chemical reaction, i.e. hydrogen abstraction by nitrogen dioxide (NO2) and the thermal decomposition of N2H4. The combustion flames uniquely comprised two types of flames, the diffusion flame and the decomposition flame. The diffusion flame came from the oxidization by NO2. The decomposition flame was caused by the heat transfer from the diffusion flame and a high rate of heat release from the thermal decomposition of N2H4. Owing to the decomposition flame, the decomposition products such as NH3, N2 and H2 became the major constituents of the downstream combustion gases. | |||||
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(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1530023014 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-14-010 |