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ロケットエンジン噴射器流れの数値解析
https://jaxa.repo.nii.ac.jp/records/6232
https://jaxa.repo.nii.ac.jp/records/6232e94e7905-9eb5-44c1-8e1e-ca8273f3aa16
名前 / ファイル | ライセンス | アクション |
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49056001.pdf (1.0 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ロケットエンジン噴射器流れの数値解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 噴射器流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 液体推薬ロケットエンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃焼室 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高圧 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 推薬燃焼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 表面張力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ナビエ-ストークス方程式 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | injector flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | liquid propellant rocket engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | combustion chamber | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high pressure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | propellant combustion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | surface tension | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Navier-Stokes equation | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Numerical study of rocket engine injector flow | |||||
著者 |
清水, 和弥
× 清水, 和弥× 清水, 太郎× Shimizu, Kazuya× Shimizu, Taro |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
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: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:宇宙輸送系基盤技術 en : JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Space Transportation Systems 巻 JAXA-SP-05-010, p. 3-8, 発行日 2006-01-20 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Numerical study on the jet flow in a high pressure fluid has been conducted in order to simulate atomization, mixing and combustion in a liquid rocket engine combustion chamber. The simulation results successfully show the break-up process of liquid oxygen jet in the high pressure hydrogen environment, while there is a little disagreement between the simulation results and theoretical estimations. Numerical results on the nitrogen jet flow agree well with the experimental results for the pressure higher than the critical point. It is suggested from the numerical results compared with experimental results that surface tension should be considered under the condition below the critical point. | |||||
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: AA0049056001 | |||||
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-05-010 |