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Vibration of thermally post-buckled composite plates embedded with shape memory alloy fibers

机译:嵌入形状记忆合金纤维的热后屈曲复合板的振动

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The vibration behavior of the thermally buckled composite plate embedded with shape memory alloy (SMA) fibers is investigated. The nonlinear finite element equations based on the first-order shear deformation plate theory are formulated for the laminated composite plate embedded with SMA fibers. The von Karman strain-displacement relation is used to account for the large deflection. The incremental method considering the influence of the initial deflections and initial stresses is adopted for the temperature-dependent material properties of SMA fibers and composite matrix. In addition, the marching method is used for determining the thermal large deflections and predicting the critical temperatures. The numerical results show the vibration characteristic of the laminated composite plate embedded with SMA fibers in the pre-buckled and post-buckled regions.
机译:研究了嵌入形状记忆合金(SMA)纤维的热屈曲复合板的振动行为。基于一阶剪切变形板理论,建立了埋入SMA纤维层合板的非线性有限元方程。 von Karman应变-位移关系用于解释大挠度。考虑到初始挠度和初始应力的影响的增量方法被用于SMA纤维和复合材料基体的温度相关材料性能。另外,行进法用于确定热大挠度并预测临界温度。数值结果显示了在预屈曲和后屈曲区域内嵌有SMA纤维的层压复合板的振动特性。

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