Aerodynamic multiobjective design exploration of flapping wing using a navier-stokes solver

Yuuki Yamazaki, Akira Oyama, Taku Nonomura, Kozo Fujii, Makoto Yamamoto

研究成果: Conference contribution

抄録

An aerodynamic design optimization problem of a three-dimensional flapping wing is explored with the multiobjective design exploration framework coupled with a Navier - Stokes solver. The results show that there is a tradeoff among lift maximization, thrust maximization, and required power minimization. The results also show that strong vortex is generated in both down stroke and up stroke motions for thrust maximization while strong vortex is generated only in down stroke motion for lift maximization. This study also reveals effects of the design parameters on the design objectives, for example, pitch offset has positive linear relationship to the lift.

本文言語English
ホスト出版物のタイトルComputational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010
出版社Kluwer Academic Publishers
ページ303-307
ページ数5
ISBN(印刷版)9783642178832
DOI
出版ステータスPublished - 2011
外部発表はい
イベント6th International Conference on Computational Fluid Dynamics, ICCFD 2010 - St. Petersburg, Russian Federation
継続期間: 2010 7月 122010 7月 16

出版物シリーズ

名前Computational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010

Other

Other6th International Conference on Computational Fluid Dynamics, ICCFD 2010
国/地域Russian Federation
CitySt. Petersburg
Period10/7/1210/7/16

ASJC Scopus subject areas

  • 流体および伝熱

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