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Effect of material nonlinearity on buckling and postbuckling of fiber composite laminated plates and cylindrical shells

机译:材料非线性对纤维复合叠层板和圆柱壳屈曲和后屈曲的影响

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An analytical study is presented in this paper on the effect of material nonlinearity on buckling and postbuckling of fiber composite laminate plates and shells subjected to general mechanical loading. The material nonlinearity of the composite is modelled by power-law type, nonlinear shear constitutive equations for each lamina. The nonlinear effective composite constitutive equations in an incremental form are incorporated into a geometrically nonlinear analysis for studying buckling and postbuckling deformations of composite laminate structures. A modified Riks' solution scheme with an updated Lagrangian formulation is used to construct the equilibrium path during composite postbuckling. Numerical examples are given to illustrate the effect of material nonlinearity on buckling load, postbuckling stiffness, and associated mode shape change of a composite structure under axial and pressure loading. Influences of lamination parameters, geometric imperfection, and loading mode on the postbuckling equilibrium path and load-bearing strength of the composite structure with the nonlinear material properties are also studied.
机译:本文针对材料非线性对承受一般机械载荷的纤维复合材料层压板和壳体的屈曲和后屈曲的影响进行了分析研究。复合材料的材料非线性是通过幂律型,每个薄片的非线性剪切本构方程来建模的。将增量形式的非线性有效复合本构方程纳入几何非线性分析中,以研究复合层合结构的屈曲和后屈曲变形。带有更新的拉格朗日公式的改进的Riks's解决方案可用于构造复合后屈曲过程中的平衡路径。数值例子说明了材料非线性对复合结构在轴向和压力载荷下的屈曲载荷,屈曲后刚度以及相关的模态形状变化的影响。研究了层合参数,几何缺陷和加载方式对材料非线性的复合结构的屈曲后平衡路径和承载强度的影响。

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