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The Instability Improvement of the Symmetric Angle-Ply and Cross-Ply Composite Plates with Shape Memory Alloy Using Finite Element Method

机译:有限元法改善形状记忆合金对称角板和交叉板复合板的不稳定性

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摘要

Shape memory alloy (SMA) wires were embedded within laminated composite plates to take advantage of the shape memory effect property of the SMA in improving post-buckling behavior of composite plates. A nonlinear finite element formulation was developed for this study. The plate-bending formulation used in this study was developed based on the first order shear deformation theory, where the von Karman's nonlinear moderate strain terms were added to the strain equations. The effect of the SMA was captured by adding recovery stress term in the constitutive equation of the SMA composite plates. Values of the recovery stress of the SMA were determined using Brinson's model. Using the principle of virtual work and the total Lagrangian approach, the final finite element nonlinear governing equation for the post-buckling of SMA composite plates was derived. Buckling and post-buckling analyses were then conducted on the symmetric angle-ply and cross-ply SMA composite plates. The effect of several parameters such as the activation temperature, volume fraction, and the initial strain of the SMA on the post-buckling behavior of the SMA composite plates were studied. It was found that significant improvements in the post-buckling behavior for composite plates can be attained.
机译:将形状记忆合金(SMA)线嵌入层压复合板中,以利用SMA的形状记忆效应特性改善复合板的后屈曲性能。为此研究开发了非线性有限元公式。本研究中使用的板弯曲公式是根据一阶剪切变形理论开发的,其中将von Karman的非线性中度应变项添加到了应变方程中。通过在SMA复合板的本构方程中添加恢复应力项来捕获SMA的效果。使用Brinson模型确定SMA的恢复应力值。利用虚拟工作原理和总拉格朗日方法,推导了SMA复合板后屈曲的最终有限元非线性控制方程。然后在对称的角度层和交叉层SMA复合板上进行屈曲和屈曲后分析。研究了SMA活化温度,体积分数和SMA初始应变等参数对SMA复合板屈曲后行为的影响。已经发现,复合板的屈曲后性能可以得到显着改善。

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