The FEA results showed that the bionic type wings has higher structure efficiency wing.
有限元分析表明,仿生型机翼具有更高的结构效能.
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The numerical simulations on free bulging were carried out by use of the FEA program ADINA.
利用非线性有限元程序ADINA对平板自由胀形进行模拟.
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以有限元分析和标准试件疲劳试验为基础,通过有限元分析的方法,细致分析了轮盘处于工作状态时,叶片榫头的接触应力对榫槽底部应力状态的影响。
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