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タービン翼の流体・熱伝導連成解析
https://jaxa.repo.nii.ac.jp/records/6635
https://jaxa.repo.nii.ac.jp/records/66358614a966-26c0-4ac8-bf1e-16b66c46ebc2
名前 / ファイル | ライセンス | アクション |
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47427034.pdf (1.9 MB)
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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 | タービン翼の流体・熱伝導連成解析 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | タービン翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 連成シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱伝導 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 有限体積法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | サブイタレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱力学的平衡 | |||||
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 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbine blade | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | coupled simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat conduction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | finite volume method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sub-iteration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermodynamic equilibrium | |||||
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 | Coupled simulation of flow and heat conduction around/inside turbine blade | |||||
著者 |
山根, 敬
× 山根, 敬× 山本, 一臣× 吉田, 豊明× Yamane, Takashi× Yamamoto, Kazuomi× Yoshida, Toyoaki |
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著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
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: 航空宇宙数値シミュレーション技術シンポジウム2003論文集 en : JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003 巻 JAXA-SP-03-002, p. 190-195, 発行日 2004-03-25 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A new coupled simulation program for flow and heat conduction has been developed based upon a common CFD platform UPACS. It connects flow calculation blocks and solid blocks without using surface temperature values explicitly. The time-lag between flow simulation and heat conduction calculation which is a severe problem in coupled simulation has been overcome by incorporating a heat conduction sub-step method. The developed program has been applied to simulations of a turbine cooling structure which are the integration of impingement and pin cooling device. | |||||
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: AA0047427034 | |||||
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-03-002 |