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ロケットエンジン供給系流れの数値解析
https://jaxa.repo.nii.ac.jp/records/6233
https://jaxa.repo.nii.ac.jp/records/623394cafabb-2604-4133-bbbb-dc2f2baa365a
名前 / ファイル | ライセンス | アクション |
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49056002.pdf (2.7 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 | ロケットエンジン供給系流れの数値解析 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | 推薬供給系 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | H-2Aロケット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スロッシング | |||||
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 | 推薬タンク | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算機プログラム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ダム崩壊問題 | |||||
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 | propellant feed system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H-2A rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sloshing | |||||
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 | propellant tank | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computer program | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | broken dam problem | |||||
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 analysis of propellant feed systems in liquid-propellant rocket engines | |||||
著者 |
根岸, 秀世
× 根岸, 秀世× 谷, 直樹× 山西, 伸宏× Negishi, Hideyo× Tani, Naoki× Yamanishi, Nobuhiro |
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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 | ||||||
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 | ||||||
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. 9-14, 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 simulator for propellant feed systems in liquid-propellant rocket engines based on CFD is under development for supporting H-2A rocket and next generation rocket development. This simulator consists of turbo pump system simulator and tank system simulator. In this paper, the tank system simulator based on CIP-LSM, which computes free surface behavior, temperature and pressure in rocket propellant tank, is presented. Also, the computed results of 2D sloshing and broken dam problems are presented to assess the accuracy of the solver for problems with strong deformation of the fluid. The results were in good agreement with other published data and experiments. As a result, it was clear that CIP-LSM is an effective method for predicting strong deformation of free surface flows. | |||||
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: AA0049056002 | |||||
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 |