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一种分析层合板大挠度动力响应的有效方法
引用本文:陈念众,张圣坤,孙海虹. 一种分析层合板大挠度动力响应的有效方法[J]. 上海交通大学学报, 2002, 36(11): 1540-1543
作者姓名:陈念众  张圣坤  孙海虹
作者单位:1. 上海交通大学,船舶与海洋工程学院,上海,200030
2. 武汉理工大学,交通学院,武汉,430063
基金项目:交通部通达计划与武汉市晨光计划资助项目
摘    要:研究了四边简支复合材料层合板在横向冲击载荷作用下的非线性大挠度动力响应,提出了一种精确的计算方法,该方法基于经典的层合板理论及板的大挠度基本假庙,得到四边简支层合板的非线性运动方程及变形协调方程;用Galerkin法进行离散,将位移和应力函数展开为级数形式,由此获得一组非线性微分方程组;引入Kronecker张量积把非线性微分方程组化为易于求解的Kronecker张量积形式的二阶常微分方程组,由4阶Runge-Kutta法数值求解,文中讨论了不同载荷形式及初始挠度对复合材料层合板动力响应的影响。

关 键 词:复合材料 层合板 初挠度 大挠度 动力响应 船舶
文章编号:1006-2467(2002)11-1540-04
修稿时间:2001-12-10

An Effective Analytical Tool for Large Deflection Dynamic Response of Composite Laminated Plates
CHEN Nian zhong ,ZHANG Sheng kun ,SUN Hai hong. An Effective Analytical Tool for Large Deflection Dynamic Response of Composite Laminated Plates[J]. Journal of Shanghai Jiaotong University, 2002, 36(11): 1540-1543
Authors:CHEN Nian zhong   ZHANG Sheng kun   SUN Hai hong
Affiliation:CHEN Nian zhong 1,ZHANG Sheng kun 1,SUN Hai hong 2
Abstract:An effective and accurate analytical tool for the nonlinear large deflection response of simply supported composite laminated plates under the action of various types of time dependent lateral loads was presented. On the basis of classical lamination theory and large deflection hypotheses of plate, the equilibrium and compatibility equations of simply supported composite laminated plates are obtained. Based on Galerkin procedure and introducing kronecker tensor product, the nonlinear partial differential equations are transformed into ordinary differential equations including kronecker tensor product by series expansion and solved numerically by fourth order Runge Kutta method. The effects of loading forms and initial geometric imperfections on the dynamic response of simply supported composite laminated plates were discussed.
Keywords:composite materials  laminate  initial geometric imperfections  large deflection  dynamic response
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