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  1. 学術雑誌論文
  2. 5 技術(工学)

Role of fluid-structure interaction in generating the characteristic tip path of a flapping flexible wing

http://hdl.handle.net/10228/00007698
http://hdl.handle.net/10228/00007698
5ac8ffd4-1fce-4f84-8729-fa9a08e71701
名前 / ファイル ライセンス アクション
10351407.pdf 10351407.pdf (7.1 MB)
アイテムタイプ 学術雑誌論文 = Journal Article(1)
公開日 2020-04-06
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_6501
資源タイプ journal article
タイトル
タイトル Role of fluid-structure interaction in generating the characteristic tip path of a flapping flexible wing
言語 en
言語
言語 eng
著者 石原, 大輔

× 石原, 大輔

WEKO 6646
e-Rad_Researcher 80363399
Scopus著者ID 56463803300
ORCiD 0000-0002-8961-2622
九工大研究者情報 255

en Ishihara, Daisuke

ja 石原, 大輔

ja-Kana イシハラ, ダイスケ


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内容記述タイプ Abstract
内容記述 This study shows that characteristic modes, such as the figure-eight mode, can be created in the path of the wing tip, which is caused by the fluid-structure interaction, using a flapping model wing with two lumped flexibilities describing the elevation motion as well as the pitching motion. A direct numerical simulation based on the three-dimensional finite element method for fluid-structure interaction (FSI) analyzes the behaviors of the model wing, the surrounding air, and their interaction, where the dynamic similarity law for the FSI is used to incorporate actual insect data, and the parallel computation algorithm is used to perform the systematic parametric study. Characteristic modes, such as the figure-eight mode, are observed in the path of the wing tip from the elevation motion of the simulated wing. This motion is considered as the forced vibration caused by the interaction with the surrounding fluid excited by the flapping of the wing. Therefore, this motion can be modulated by the flexibility to change the natural frequency, which can be controlled by the muscles at the base of the wing in the actual insect. The present simulation shows that the selection between these modes in the path of the wing tip depends on the ratio between the natural frequency of the elevation motion and the flapping frequency. In the case of the figure eight, the upward elevation motion of the wing acts on the leading-edge vortex (LEV) so as to keep its momentum upon stroke reversal. Therefore, this LEV can remain in the wake of the wing after stroke reversal and enhance the next LEV. Because of this effect, the lift increases significantly as the mode of the wing tip path shifts to the figure-eight mode. This understanding will contribute to a developed field of bioinspired micro air vehicles; i.e., it will reduce the complexity of electromechanical devices that prescribe entire motions of their wings.
言語 en
書誌情報 en : Physical Review E

巻 98, 号 3, p. 032411-1, 発行日 2018-09-17
出版社
出版者 American Physical Society
言語 en
DOI
関連タイプ isVersionOf
識別子タイプ DOI
関連識別子 https://doi.org/10.1103/PhysRevE.98.032411
ISSN
収録物識別子タイプ PISSN
収録物識別子 2470-0045
ISSN
収録物識別子タイプ EISSN
収録物識別子 2470-0053
著作権関連情報
権利情報 Copyright (c) 2018 American Physical Society
出版タイプ
出版タイプ AM
出版タイプResource http://purl.org/coar/version/c_ab4af688f83e57aa
査読の有無
値 yes
研究者情報
URL https://hyokadb02.jimu.kyutech.ac.jp/html/255_ja.html
論文ID(連携)
値 10351407
連携ID
値 8203
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