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径向载荷作用下复合材料圆柱壳的非线性动力屈曲
引用本文:唐文勇,王天霖,张圣坤. 径向载荷作用下复合材料圆柱壳的非线性动力屈曲[J]. 振动与冲击, 2006, 25(2): 155-158
作者姓名:唐文勇  王天霖  张圣坤
作者单位:上海交通大学,船舶海洋与建筑工程学院,上海,200030
基金项目:中国科学院资助项目;上海市高校优秀青年教师后备人选基金
摘    要:采用半解析法求解径向阶跃载荷作用下复合材料圆柱壳的非线性动力屈曲。基于一阶剪切变形理论,由Hamilton原理推导出包含横向剪切变形以及几何初缺陷的圆柱壳的非线性动力方程,位移及载荷沿周向采用级数展开,由Galerkin方法得到微分方程组,通过有限差分法求解;根据响应情况,由B—R准则判定屈曲,确定屈曲临界载荷。

关 键 词:复合材料  圆柱壳  非线性  动力屈曲  半解析法
收稿时间:2005-10-09
修稿时间:2005-12-01

Nonlinear Dynamic Buckling of Composite Cylindrical Shells under Radial Loads
Tang Wenyong,Wang Tianlin,Zhang Shenkun. Nonlinear Dynamic Buckling of Composite Cylindrical Shells under Radial Loads[J]. Journal of Vibration and Shock, 2006, 25(2): 155-158
Authors:Tang Wenyong  Wang Tianlin  Zhang Shenkun
Abstract:The nonlinear dynamic buckling of a laminated composite cylindrical shell under radial step loading is solved by the semi-analytical method in this paper. Based on the first order shear deformation theory, the nonlinear dynamic equations including transverse shear deformation and initial geometric imperfections are obtained by Hamilton's principle . The nonlinear partial differential equations are transformed to ordinary differential equations by the Fourier series expansion of displacement and load in along circumference and using Galerkin's method, the ordinary differential eguations are solved by the finite difference method. The buckling is judged from responses by B-R criterion and critical loads are determined.
Keywords:composite materials   cylindrical shell   non-linear   dynamic buckling   semi-analytical method
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