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  1. 060 工学部・工学研究科 = Faculty of Engineering
  2. 060 学術雑誌論文 = Articles in academic journal

Aeroelastic Effect of Corrugation for an Insect-Sized Flapping Wing

http://hdl.handle.net/10069/00041545
http://hdl.handle.net/10069/00041545
baf99546-dd12-4374-ba94-82224ec05206
名前 / ファイル ライセンス アクション
AIAAJ60_3180.pdf AIAAJ60_3180.pdf (1.7 MB)
アイテムタイプ 学術雑誌論文 / Journal Article(1)
公開日 2022-05-24
タイトル
タイトル Aeroelastic Effect of Corrugation for an Insect-Sized Flapping Wing
言語
言語 eng
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
著者 Minoda, Takeshi

× Minoda, Takeshi

Minoda, Takeshi

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Nagai, Hiroto

× Nagai, Hiroto

Nagai, Hiroto

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Yashiro, Shigeki

× Yashiro, Shigeki

Yashiro, Shigeki

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Uda, Nobuhide

× Uda, Nobuhide

Uda, Nobuhide

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抄録
内容記述タイプ Abstract
内容記述 The fundamental aeroelastic effect of the corrugation of an insect-sized simple flapping wing is numerically investigated. A baseline model for a corrugated flapping wing is constructed such that the balance among the aerodynamic, elastic, and inertial forces acting on the wing matches that acting on insect wings in accordance with the measured material properties of insect wings. The thickness of the corrugated airfoil and the amplitude of corrugation are systematically varied around the baseline to modulate both the natural frequencies and mode shapes. Unsteady aeroelastic simulation based on three-dimensional Naiver–Stokes equations is conducted for the corrugated flapping wings. The numerical simulation is validated by measuring the natural frequency and mean lift of corrugated flapping wings. The results indicate that the corrugation of insect flapping wings is aeroelastically effective in providing both an appropriate passive deformation and a light-weight wing. To maximize the hovering efficiency, the optimal amplitude of corrugation is 1.7 to 2.6% of the chord length, the wing mass ratio is 0.7 to 1.5, and the natural frequency is 2.1 to 2.6 times as large as the input flapping frequency. These optimal design parameters are close to (but slightly smaller than) those of insect wings.
書誌情報 AIAA Journal

巻 60, 号 5, p. 3180-3193, 発行日 2022-02-11
出版者
出版者 AIAA International
ISSN
収録物識別子タイプ ISSN
収録物識別子 0001-1452
DOI
関連タイプ isVersionOf
識別子タイプ DOI
関連識別子 10.2514/1.J061027
権利
権利情報 © 2021 by Hiroto Nagai. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
著者版フラグ
出版タイプ AM
出版タイプResource http://purl.org/coar/version/c_ab4af688f83e57aa
引用
内容記述タイプ Other
内容記述 AIAA Journal, 60(5), pp. 3180-3193; 2022
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