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  1. 060 工学部
  2. 0601 学術論文

Aerodynamic comparison of a butterfly-like flapping wing-body model and a revolving-wing model

http://hdl.handle.net/10091/00022525
61616ced-d624-434b-91c8-98747cd593d1
名前 / ファイル ライセンス アクション
16K18012_05.pdf 16K18012_05.pdf (5.5 MB)
Item type 学術雑誌論文 / Journal Article(1)
公開日 2021-02-16
タイトル
言語 en
タイトル Aerodynamic comparison of a butterfly-like flapping wing-body model and a revolving-wing model
言語
言語 eng
キーワード
主題Scheme Other
主題 flapping wing
キーワード
主題Scheme Other
主題 revolving wing
キーワード
主題Scheme Other
主題 aerodynamic performance
キーワード
主題Scheme Other
主題 lattice Boltzmann method
キーワード
主題Scheme Other
主題 immersed boundary method
資源タイプ
資源 http://purl.org/coar/resource_type/c_6501
タイプ journal article
著者 Suzuki, Kosuke

× Suzuki, Kosuke

WEKO 110288

Suzuki, Kosuke

Search repository
Yoshino, Masato

× Yoshino, Masato

WEKO 110289

Yoshino, Masato

Search repository
信州大学研究者総覧へのリンク
氏名 Suzuki, Kosuke
URL https://soar-rd.shinshu-u.ac.jp/profile/ja.uayebUkh.html
信州大学研究者総覧へのリンク
氏名 Yoshino, Masato
URL https://soar-rd.shinshu-u.ac.jp/profile/ja.ONkpbpkh.html
出版者
出版者 IOP PUBLISHING LTD
引用
内容記述タイプ Other
内容記述 FLUID DYNAMICS RESEARCH.49(3):035512(2017)
書誌情報 FLUID DYNAMICS RESEARCH

巻 49, 号 3, p. 035512, 発行日 2017-05-11
抄録
内容記述タイプ Abstract
内容記述 The aerodynamic performance of flapping- and revolving-wing models is investigated by numerical simulations based on an immersed boundary-lattice Boltzmann method. As wing models, we use (i) a butterfly-like model with a body and flapping- rectangular wings and (ii) a revolving-wing model with the same wings as the flapping case. Firstly, we calculate aerodynamic performance factors such as the lift force, the power, and the power loading of the two models for Reynolds numbers in the range of 50-1000. For the flapping-wing model, the power loading is maximal for the maximum angle of attack of 90 degrees, a flapping amplitude of roughly 45 degrees, and a phase shift between the flapping angle and the angle of attack of roughly 90 degrees. For the revolving-wing model, the power loading peaks for an angle of attack of roughly 45 degrees. In addition, we examine the ground effect on the aerodynamic performance of the revolving-wing model. Secondly, we compare the aerodynamic performance of the flapping- and revolving-wing models at their respective maximal power loadings. It is found that the revolving-wing model is more efficient than the flapping- wing model both when the body of the latter is fixed and where it can move freely. Finally, we discuss the relative agilities of the flapping- and revolving-wing models.
資源タイプ(コンテンツの種類)
内容記述タイプ Other
内容記述 Article
ISSN
収録物識別子タイプ ISSN
収録物識別子 0169-5983
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AA10686129
DOI
関連識別子
識別子タイプ DOI
関連識別子 https://doi.org/10.1088/1873-7005/aa6b78
関連名称
関連名称 10.1088/1873-7005/aa6b78
権利
権利情報 This is the Accepted Manuscript version of an article accepted for publication in FLUID DYNAMICS RESEARCH. IOP Publishing Ltd is not responsible for any errors or omissions in this version of the manuscript or any version derived from it. The Version of Record is available online at https://doi.org/10.1088/1873-7005/aa6b78.© 2017. This manuscript version is made available under the CC-BY-NC-ND 4.0 license http://creativecommons.org/licenses/by-nc-nd/4.0/.
出版タイプ
出版タイプ AM
出版タイプResource http://purl.org/coar/version/c_ab4af688f83e57aa
WoS
表示名 Web of Science
URL http://gateway.isiknowledge.com/gateway/Gateway.cgi?&GWVersion=2&SrcAuth=ShinshuUniv&SrcApp=ShinshuUniv&DestLinkType=FullRecord&DestApp=WOS&KeyUT=000403345500001
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