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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 5.9 ) Pub Date : 2023-11-02 , DOI: 10.1080/19942060.2023.2271053 Rashmikant 1 , M. Onishi 1 , K. Sugikawa 1 , D. Ishihara 1
Engineering Applications of Computational Fluid Mechanics ( IF 5.9 ) 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:
利用非线性动力和流固耦合分析的分层耦合对扑翼纳米飞行器的飞行性能进行计算评估
本研究致力于引入一种创新的分层耦合方法,利用先进的技术来评估聚合物微机械扑翼纳米飞行器(FWNAV)的飞行能力。
更新日期:2023-11-03
中文翻译:
利用非线性动力和流固耦合分析的分层耦合对扑翼纳米飞行器的飞行性能进行计算评估
本研究致力于引入一种创新的分层耦合方法,利用先进的技术来评估聚合物微机械扑翼纳米飞行器(FWNAV)的飞行能力。