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  1. 学術雑誌論文
  2. 5 技術(工学)

2.5-dimensional insect-mimetic wing model for flapping wing nano air vehicles and design window search for manufacturable solutions using polymer micromachining

http://hdl.handle.net/10228/0002000312
http://hdl.handle.net/10228/0002000312
8ea9c6bf-2a51-4632-aae4-5cdf36639e6b
名前 / ファイル ライセンス アクション
10401551.pdf 10401551.pdf (2 MB)
アイテムタイプ 学術雑誌論文 = Journal Article(1)
公開日 2023-12-07
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 2.5-dimensional insect-mimetic wing model for flapping wing nano air vehicles and design window search for manufacturable solutions using polymer micromachining
言語 en
言語
言語 eng
著者 Shankar, Vinay

× Shankar, Vinay

en Shankar, Vinay

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Matsuo, Ryunosuke

× Matsuo, Ryunosuke

en Matsuo, Ryunosuke

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Onishi, Minato

× Onishi, Minato

en 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


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内容記述タイプ Abstract
内容記述 Insect flapping wings undergo large deformations such as feathering and cambering for creating large thrust forces. Hence, insect-mimetic wings for flapping wing nano air vehicles (FWNAVs) will replicate these characteristic deformations. For the purpose of realizing this type of wings, in this study, a 2.5-dimensional (2.5-D) insect-mimetic wing model for FWNAVs is proposed. The proposed wing model consists of the leading-edge, the central vein, the root vein, and the membrane, all of which are described by shell elements. The feathering and cambering of the proposed wing model can be caused by the aerodynamic pressure. Furthermore, the proposed wing can be fabricated using polymer micromachining because of the complete 2.5-D structure. In order to demonstrate these capabilities, we perform the design window (DW) search. The DW is defined as the existing area of satisfactory design solutions in the design parameter space, where each solution can produce a sufficient camber. The DWs for the leading-edge, the central and root veins are searched continuously using the geometrically nonlinear finite element analysis under quasi-steady aerodynamic modeling. The thickness is chosen as the design parameter, while the other parameters are set following actual insects and polymer materials. Finally, we determine the final solutions from the DWs for a specific polymer micromachining technique. In our future work, the proposed solutions will be manufactured for the future miniaturization of FWNAVs.
言語 en
備考
内容記述タイプ Other
内容記述 2022 IEEE 17th International Conference on Nano/Micro Engineered and Molecular Systems (NEMS), IEEE NEMS 2022, April 14-17, 2022, Taoyuan, Taiwan
言語 en
書誌情報 en : 2022 IEEE 17th International Conference on Nano/Micro Engineered and Molecular Systems (NEMS)

p. 306-311, 発行日 2022-06-10
出版社
出版者 IEEE
DOI
関連タイプ isVersionOf
識別子タイプ DOI
関連識別子 https://doi.org/10.1109/NEMS54180.2022.9791094
ISBN
関連タイプ isVersionOf
識別子タイプ ISBN
関連識別子 978-1-6654-8301-8
ISBN
関連タイプ isVersionOf
識別子タイプ ISBN
関連識別子 978-1-6654-8302-5
ISSN
収録物識別子タイプ EISSN
収録物識別子 2474-3755
ISSN
収録物識別子タイプ PISSN
収録物識別子 2474-3747
著作権関連情報
権利情報 Copyright (c) 2022 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.
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
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