机翼/机身结构 WING/FUSELAGE STRUCTURE ; WING
The results show that this method can solve the optimization problem of wing structure with uncertainties efficiently,is convenient to be applied to software integration and is suitable for large complex structural model.
研究显示,该方法切实可行,能有效解决机翼结构不确定性优化中计算量大、失效功能函数不能显式表达的问题,并且该方法适用于大型复杂模型,方便软件集成。
参考来源 - 具有随机不确定性的机翼颤振优化·2,447,543篇论文数据，部分数据来源于NoteExpress
试验结果表明，机翼结构的设计满足了设计要求。
The results of the experiment show that the design of the wing structure satisfies the design requirements.
应用该结构模型可以很好的模拟机翼结构的实际情况。
With use of this structure model, we can simulate the real performance of aerofoil very well.
为机翼结构的可靠性分析和损伤容限设计提供了比较有价值的力学分析手段。
A good mechanics analysis approach was presented for reliability analysis and damage tolerance design of aerofoil structure.
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