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ガスタービン設計における構造解析の現状
https://jaxa.repo.nii.ac.jp/records/6612
https://jaxa.repo.nii.ac.jp/records/661222e8fb03-3a63-464c-a7a9-237d0e8ec72b
名前 / ファイル | ライセンス | アクション |
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47427011.pdf (1.4 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 | ガスタービン設計における構造解析の現状 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ガスタービン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 構造設計 | |||||
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 | コスト削減 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 構造解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ロータダイナミクス | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | き裂伸展解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 塑性変形 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | gas turbine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | structural design | |||||
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 | cost reduction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | structural analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rotor dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | crack growth analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | plastic deformation | |||||
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 | Latest status of numerical simulation for aero-engine structural design | |||||
著者 |
藤村, 哲司
× 藤村, 哲司× 篠崎, 正治× Fujimura, Tetsuji× Shinozaki, Masaharu |
|||||
著者所属 | ||||||
石川島播磨重工業 航空宇宙事業本部 技術開発センター | ||||||
著者所属 | ||||||
石川島播磨重工業 航空宇宙事業本部 技術開発センター | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co. Ltd. Research & Engineering Center, Aero-Engine & Space Operations | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co. Ltd. Research & Engineering Center, Aero-Engine & Space Operations | ||||||
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. 59-64, 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 | Recently, cutting aero-engine development cycle times is being pursued aggressively to reduce program risk as well as total amount of costs. Under such a back ground with very rapid progress of computer utilization environment, numerical simulations have been extensively applied to aero-engine structural design. From the viewpoint of recent trend of advanced detailed and multidisciplinary design approach, detailed non-linear finite element analysis, rotor dynamics, crack growth analysis and impact analysis are presented. | |||||
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: AA0047427011 | |||||
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 |