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  1. 学術雑誌論文
  2. 4 自然科学

Partitioned Method of Insect Flapping Flight for Maneuvering Analysis

http://hdl.handle.net/10228/00007693
http://hdl.handle.net/10228/00007693
86501b1b-69f9-4de4-9073-8b69fd99c2a0
名前 / ファイル ライセンス アクション
cmes.2019.06781.pdf cmes.2019.06781.pdf (1.8 MB)
アイテムタイプ 学術雑誌論文 = Journal Article(1)
公開日 2020-04-03
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 Partitioned Method of Insect Flapping Flight for Maneuvering Analysis
言語
言語 eng
著者 Onishi, Minato

× Onishi, Minato

WEKO 27291

Onishi, Minato

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石原, 大輔

× 石原, 大輔

WEKO 6646
e-Rad 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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抄録
内容記述タイプ Abstract
内容記述 This study proposed a partitioned method to analyze maneuvering of insects during flapping flight. This method decomposed the insect flapping flight into wing and body subsystems and then coupled them via boundary conditions imposed on the wing’s base using one-way coupling. In the wing subsystem, the strong coupling of the flexible wings and surrounding fluid was accurately analyzed using the finite element method to obtain the thrust forces acting on the insect’s body. The resulting thrust forces were passed from the wing subsystem to the body subsystem, and then rigid body motion was analyzed in the body subsystem. The rolling, yawing, and pitching motions were simulated using the proposed method as follows: In the rolling simulation, the difference of the stroke angle between the right and left wings caused a roll torque. In the yawing simulation, the initial feathering angle in the right wing only caused a yaw torque. In the pitching simulation, the difference between the front- and back-stroke angles in both the right and left wings caused a pitch torque. All three torques generated maneuvering motion comparable with that obtained in actual observations of insect flight. These results demonstrate that the proposed method can adequately simulate the fundamental maneuvers of insect flapping flight. In the present simulations, the maneuvering mechanisms were investigated at the governing equation level, which might be difficult using other approaches. Therefore, the proposed method will contribute to revealing the underlying insect flight mechanisms.
書誌情報 Computer Modeling in Engineering & Sciences

巻 121, 号 1, p. 145-175, 発行日 2019
出版社
出版者 Tech Science Press
DOI
関連タイプ isIdenticalTo
識別子タイプ DOI
関連識別子 info:doi/10.32604/cmes.2019.06781
NCID
収録物識別子タイプ NCID
収録物識別子 AA11491034
ISSN
収録物識別子タイプ ISSN
収録物識別子 1526-1492
ISSN
収録物識別子タイプ ISSN
収録物識別子 1526-1506
出版タイプ
出版タイプ VoR
出版タイプResource http://purl.org/coar/version/c_970fb48d4fbd8a85
査読の有無
値 yes
研究者情報
URL https://hyokadb02.jimu.kyutech.ac.jp/html/255_ja.html
連携ID
値 8197
情報源
識別子タイプ URI
関連識別子 doi:10.32604/cmes.2019.06781
関連名称 doi:10.32604/cmes.2019.06781
情報源
識別子タイプ URI
関連識別子 http://www.techscience.com/journal/CMES
関連名称 http://www.techscience.com/journal/CMES
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