WEKO3
アイテム
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ITBL上での空力/構造解析を組み合わせた翼振動応答予測
https://jaxa.repo.nii.ac.jp/records/6469
https://jaxa.repo.nii.ac.jp/records/646960ed611e-c4be-483b-bd62-5e628b8250cb
名前 / ファイル | ライセンス | アクション |
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48469029.pdf (2.4 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 | ITBL上での空力/構造解析を組み合わせた翼振動応答予測 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 予測 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 強制振動 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 構造振動 | |||||
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 | 構造解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧縮機翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非定常空気力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 後流干渉 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | prediction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | forced vibration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | structural vibration | |||||
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 | structural analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | compressor blade | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unsteady aerodynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wake interaction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
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 | Prediction of blade forced response by use of a combination of aerodynamic and structural analysis on ITBL network | |||||
著者 |
浜辺, 正昭
× 浜辺, 正昭× 大庭, 芳則× 児玉, 秀和× 吉田, 正廣× 山本, 一臣× Hamabe, Masaaki× Oba, Yoshinori× Kodama, Hidekazu× Yoshida, Masahiro× Yamamoto, Kazuomi |
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著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
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2004論文集 en : JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004 巻 JAXA-SP-04-012, p. 172-177, 発行日 2005-03-25 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A numerical analysis system has been developed for predicting forced vibration levels of compressor blades of a given blade row subjected to either wakes from an upstream blade row or potential flow disturbances from an upstream/downstream blade row. The system consists of an unsteady aerodynamic analysis and a structural analysis. The unsteady aerodynamic analysis based on an unsteady three-dimensional multi-blade row Reynolds-averaged Navier-Stokes analysis is performed to predict the unsteady aerodynamic load in a multi-blade row environment. The structural analysis using a finite element model is performed to get the mode shape and frequency of the blade. In this paper, the system is established on ITBL (IT-Based Laboratory) network, and applied to a rotor blade of High-Pressure Compressor. As a result, it is found that the pressure perturbation on a rotor blade is to be three-dimensional distribution and vary from blade to blade. | |||||
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: AA0048469029 | |||||
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-04-012 |