某型飞机发动机短舱结构设计
Trainer(2013)
Abstract
针对某型飞机的特点,提出了该发动机固定短舱主传力结构的设计方案,并用MSC/Patran软件进行了有限元分析;根据计算结果,结合发动机的安装和维护要求,对方案进行逐步优化并确定最终方案。
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Key words
finite element analysis,optimized,Engine nacelle
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