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Multiscale studies on the nonlinear vibration of delaminated composite laminates–global vibration mode with micro buckles on the interfaces

机译:分层复合材料层合板非线性振动的多尺度研究–界面处带有微扣的整体振动模式

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摘要

This paper presents a multiscale approach to study the nonlinear vibration of fiber reinforced composite laminates containing an embedded, through-width delamination dividing the laminate into four sub-laminates. The equations of motion are established from macroscopic nonlinear mechanics for plates and shells and micro-mechanics of composite material to allow for the influences of large amplitude, membrane stretching in the neutral plane, and the interactions of the sublaminates. Analytical solutions obtained in this paper reveal that the interaction penalty at the interfaces plays a coupling effect between sublaminates, which eventually alters the vibration characters of the four-sublaminate lamina in macroscopic and microscopic mechanism. From a macro perspective, sub-laminates above and below the delamination vibrate in exactly the same mode in spite of their different stiffness and the four-sublaminate lamina has a consistent global vibration mode. In accompanying with the macro vibration, micro buckles occur on the interfaces of the delamination with amplitude about 10−3 times of that of the global mode. It is found that the vibration frequency is an eigenvalue of the delaminated lamina determined only by the geometry of the delamination. Authentication of the multiscale study is fulfilled by comparing the analytical solutions with the FEA results.
机译:本文提出了一种多尺度方法来研究纤维增强复合材料层压板的非线性振动,该层压板包含一个嵌入的,贯穿宽度的分层,将该层压板分为四个子层压板。运动方程由板和壳的宏观非线性力学以及复合材料的微力学建立,以考虑大振幅,中性面膜拉伸以及层合体相互作用的影响。本文得到的解析解表明,界面处的相互作用罚分在层合板之间起耦合作用,最终改变了宏观和微观机制下四层合板的振动特性。从宏观的角度来看,分层结构之上和之下的子层压板尽管具有不同的刚度,但仍以完全相同的模式振动,而四子层压板的层板具有一致的整体振动模式。伴随宏观振动,分层的界面上会出现微弯曲,其振幅约为整体模式的10 -3 倍。已经发现,振动频率是仅由分层的几何形状确定的分层的特征值。通过将分析解决方案与FEA结果进行比较,可以完成对多尺度研究的认证。

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