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MHIにおける空力弾性応答解析について
https://jaxa.repo.nii.ac.jp/records/6615
https://jaxa.repo.nii.ac.jp/records/661587a189c7-2a7a-4706-9cad-f1440dfaad97
名前 / ファイル | ライセンス | アクション |
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47427014.pdf (588.8 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 | MHIにおける空力弾性応答解析について | |||||
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 | 航空機設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷音速飛行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷音速フラッタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | SST | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層剥離 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高アスペクト比翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速飛行 | |||||
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 | aircraft design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transonic flight | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transonic flutter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SST | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer separation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high aspect ratio wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic flight | |||||
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 | MHI activities on aeroelastic analysis | |||||
著者 |
野村, 隆之
× 野村, 隆之× 柳川, 祐輝× Nomura, Takayuki× Yanagawa, Hiroki |
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著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
日本航空機開発協会 | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aircraft Development Corporation | ||||||
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. 75-80, 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 | MHI activities on aeroelasticity and the associated fields are presented. MHI has conducted many types of aeroelastic analysis throughout the development of aircraft in the past decades. The transonic dip phenomenon is one of the most important items in the aeroelasticity field and cannot be analyzed by the linear aerodynamics tools commonly used in the aircraft design. The recent progress in the time-marching method that calculates the flow field around the airfoil in the time domain enables solving the transonic dip by the analysis. In this paper, two analysis examples using USTF3 developed at NAL are presented that studied the transonic flutter properties of the high-aspect-ratio transport wing and SST wing, both of which were done in the design phase at MHI. | |||||
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: AA0047427014 | |||||
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 |