Structural Design Optimization of Commercial Aircraft WIng 模型预览

GrabCAD 模型信息

Structural Design Optimization of Commercial Aircraft WIng · 模型 240419

作者:Ganesh Raj

 Designed an aircraft wing with all structural integrated components  Generated real time wind load from CFD software for load conditions  Analyzed the designed component with mapped loads in FEA  Optimized ribs according to stress response to reduce the weight Tools Used: CATIA,Unigraphics, Hypermesh,RADIOSS,OPTISTRUCT,STAR CCM+

格式
Rendering、STEP / IGES
分类
Aerospace、Aviation、Educational
标签
未标注
数据更新
2026-10-30T09:21:28Z
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