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非構造格子を用いた2次元フラッタ解析
https://jaxa.repo.nii.ac.jp/records/6638
https://jaxa.repo.nii.ac.jp/records/6638c4024171-4434-4ae8-a241-a2b392bb3d5e
名前 / ファイル | ライセンス | アクション |
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47427037.pdf (785.1 kB)
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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 | 非構造格子を用いた2次元フラッタ解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力弾性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フラッタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2次元モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非構造格子 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 移動境界 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 臨界動圧 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 有限差分法 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aeroelasticity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flutter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two dimensional model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unstructured grid | |||||
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 | moving boundary | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | critical dynamic pressure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | finite difference method | |||||
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 | Two-dimensional flutter analysis using unstructured grids | |||||
著者 |
塚田, はるみ
× 塚田, はるみ× 宮路, 幸二× Tsukada, Harumi× Miyaji, Koji |
|||||
著者所属 | ||||||
横浜国立大学 大学院 | ||||||
著者所属 | ||||||
横浜国立大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Yokohama National University Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
Yokohama National University | ||||||
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. 208-213, 発行日 2004-03-25 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Two-dimensional aeroelastic problems at supersonic/transonic speeds are numerically simulated. Simplified structural computations are coupled with CFD code using unstructured grids with moving boundary. In panel flutter analyses, elastic deformations are treated as a one-dimensional beam problem and the equation is solved by the finite difference method. In wing flutter analyses, a well-known bending-torsion model with two degrees of freedom is used. Both simulation results well predict flutter boundaries, namely, critical dynamic pressure or flow speeds across which flutter occurs and the accuracy of the developed method has been proved. | |||||
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: AA0047427037 | |||||
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 |