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Aerodynamic comparison of a butterfly-like flapping wing-body model and a revolving-wing model
http://hdl.handle.net/10091/00022525
http://hdl.handle.net/10091/0002252561616ced-d624-434b-91c8-98747cd593d1
名前 / ファイル | ライセンス | アクション |
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16K18012_05.pdf (5.5 MB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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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 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | https://doi.org/10.1088/1873-7005/aa6b78 | |||||
関連名称 | 10.1088/1873-7005/aa6b78 | |||||
キーワード | ||||||
主題 | flapping wing, revolving wing, aerodynamic performance, lattice Boltzmann method, 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× Yoshino, Masato |
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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 |
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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 | |||||
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 |