Finite Element Framework for Efficient Design of Three Dimensional Multicomponent Composite Helicopter Rotor Blade System

In the present study, a three-dimensional finite element framework has been developed to model a full-scale multilaminate composite helicopter rotor blade. Tip deformation and stress behavior have been analyzed for external aerodynamic loading conditions and compared with the Abaqus FEA model. Furth...

詳細記述

書誌詳細
第一著者: Arunabha M. Roy
フォーマット: 論文
言語:English
出版事項: MDPI AG 2021-03-01
シリーズ:Eng
主題:
オンライン・アクセス:https://www.mdpi.com/2673-4117/2/1/6