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Passive and active piezoelectric effects on flutter suppression of highly flexible wings
https://jaxa.repo.nii.ac.jp/records/3399
https://jaxa.repo.nii.ac.jp/records/3399d1292505-71e9-4aa1-818f-2fd0688e7efd
名前 / ファイル | ライセンス | アクション |
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AA1630046006.pdf (1.2 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2017-04-27 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Passive and active piezoelectric effects on flutter suppression of highly flexible wings | |||||
言語 | ||||||
言語 | eng | |||||
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 | Multifunctional structure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Active control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Energy harvesting | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Slender wing | |||||
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 |
津島, 夏輝
× 津島, 夏輝× Su, Weihua× Tsushima, Natsuki× Su, Weihua |
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著者所属(英) | ||||||
en | ||||||
University of Alabama | ||||||
著者所属(英) | ||||||
en | ||||||
University of Alabama | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
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 the First International Symposium on Flutter and its Application 巻 JAXA-SP-16-008E, p. 67-76, 発行日 2017-03-15 |
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会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | First International Symposium on Flutter and its Application (May 15-17, 2016. Mielparque-tokyo), Minato-ku, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The paper addresses both active and passive flutter suppression for highly flexible wings using piezoelectric transduction. The piezoelectric effect is included in a strain-based geometrically nonlinear beam formulation. The resulting structural dynamic equations for multifunctional beams are then coupled with a finite-state unsteady aerodynamic formulation, allowing for piezoelectric energy harvesting and actuation with the nonlinear aeroelastic system. With the development, it is possible to provide an integral aeroelastic and electromechanical solution of concurrent active piezoelectric control on and energy harvesting from wing vibrations, with the consideration of the geometrical nonlinear effects of the slender multifunctional wings. The energy harvesting system can provide an additional damping effect on the wing as well as its harvesting capability. In this paper, an LQG controller is developed for the active control of wing limit-cycle oscillations due to the onset of flutter instability. The controller demonstrates effective flutter control capability. Furthermore, a concurrent active vibration control and energy harvesting can also be realized for the multifunctional wing system with embedded piezoelectric materials. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
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: AA1630046006 | |||||
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-16-008E |