Buckling Analysis of Composite Laminate Plates Based on the n-order Shear Deformation Theory
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摘要: 采用n阶剪切变形理论分析了复合材料层合板的屈曲问题,根据虚功原理推导出了复合材料层合板在面内载荷作用下临界屈曲的控制微分方程.将此方法所得结果与其他文献中的结果进行了比较,结果表明,该理论具有较高的计算精度.Abstract: The buckling of composite laminate plates was analyzed with the nth-order shear deformation theory. The virtual work principle was used to derive the governing equations for the critical buckling of laminate pates under in-plane loads. The comparison between the present results and the results of previous literatures shows good agreement and high calculation accuracy.
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