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Flutter LCO in isentropic flow: Analytical theory
https://jaxa.repo.nii.ac.jp/records/5662
https://jaxa.repo.nii.ac.jp/records/56621774029e-11b0-40f7-a1c2-242f69b59f45
名前 / ファイル | ライセンス | アクション |
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63824007.pdf (399.7 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 | ||||||
言語 | en | |||||
タイトル | Flutter LCO in isentropic flow: Analytical theory | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2次元流 | |||||
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 | フラッタ解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 等エントロピー流 | |||||
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 | 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 | 航空機構造 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼振動 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | リミットサイクル振動 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非線形性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 分岐 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two dimensional flow | |||||
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 | flutter analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | isentropic flow | |||||
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 | 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 | aircraft structure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wing oscillation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | limit cycle oscillation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nonlinearity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | bifurcation | |||||
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 | |||||
著者 |
Balakrishnan, A. V.
× Balakrishnan, A. V. |
|||||
著者所属 | ||||||
University of California, Los Angeles Flight Systems Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
University of California, Los Angeles Flight Systems Research Center | ||||||
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 en : JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling 巻 JAXA-SP-07-008E, p. 64-76, 発行日 2008-02-29 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Using full continuum models, we establish purely theoretically that in two-dimensional isentropic flow, the flutter speed for a slender high-aspect ratio wing is a Hopf bifurcation point of the aeroelastic structure dynamics which can be expressed as a non-linear convolution evolution equation. The flutter speed is determined by the linearized model and the LCO (Limit Cycle Oscillation) is periodic with period (2 pi/omega) where omega is the angular flutter frequency in the linear model, and can be expressed as a harmonic series. | |||||
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: AA0063824007 | |||||
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-07-008E |