Computational evaluation of flight performance of flapping-wing nano air vehicles using hierarchical coupling of nonlinear dynamic and fluid-structure interaction analyses,Engineering Applications of Computational Fluid Mechanics

当前位置： X-MOL 学术 › Eng. Appl. Comput. Fluid Mech. › 论文详情

Our official English website, www.x-mol.net, welcomes your feedback! (Note: you will need to create a separate account there.)

Computational evaluation of flight performance of flapping-wing nano air vehicles using hierarchical coupling of nonlinear dynamic and fluid-structure interaction analyses
Engineering Applications of Computational Fluid Mechanics ( IF 6.1 ) Pub Date : 2023-11-02 , DOI: 10.1080/19942060.2023.2271053
Rashmikant ₁ , M. Onishi ₁ , K. Sugikawa ₁ , D. Ishihara ₁

Affiliation

This study endeavours to introduce an inventive hierarchical coupling methodology for evaluating the flight capabilities of polymer micromachined flapping-wing nano air vehicles (FWNAVs) using adva...

中文翻译：