首页 | 本学科首页   官方微博 | 高级检索  
     

半解析法求解复合材料圆柱壳的非线性动力响应
引用本文:王天霖,唐文勇,张圣坤. 半解析法求解复合材料圆柱壳的非线性动力响应[J]. 上海交通大学学报, 2005, 39(11): 1851-1855
作者姓名:王天霖  唐文勇  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;上海交通大学,船舶海洋与建筑工程学院,上海,200030;上海交通大学,船舶海洋与建筑工程学院,上海,200030
基金项目:国家自然科学基金资助项目(10202013);上海市高校优秀青年教师后备人选项目资助.
摘    要: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始缺陷的圆柱壳的非线性动力方程,并用半解析法求解;位移及载荷沿周向傅里叶级数展开,由Galerkin方法得到微分方程组,通过有限差分法求解.讨论了径向载荷作用下的复合材料圆柱壳的动力响应问题.

关 键 词:复合材料  圆柱壳  非线性  动力响应  半解析法
文章编号:1006-2467(2005)11-1851-05
收稿时间:2004-12-13
修稿时间:2004-12-13

The Semi-analytical Method to Solve Dynamic Response of Composite Cylindrical Shell
WANG Tian-lin,TANG Wen-yong,ZHANG Sheng-kun. The Semi-analytical Method to Solve Dynamic Response of Composite Cylindrical Shell[J]. Journal of Shanghai Jiaotong University, 2005, 39(11): 1851-1855
Authors:WANG Tian-lin  TANG Wen-yong  ZHANG Sheng-kun
Affiliation:School of Naval Architecture,Ocean and Civil Eng. , Shanghai Jiaotong Univ. , Shanghai 200030,China
Abstract:Based on the first order shear deformation theory,the nonlinear dynamic equations including transverse shear deformation and initial geometric imperfections were obtained by Hamilton's principle and solved by the semi-analytical method.The nonlinear partial differential equations are transformed to ordinary differential equations by the expansion of displacement and load in Fourier series along circumference,which are numerically solved by finite difference method.The dynamic response of laminated composite cylindrical shell was discussed.
Keywords:composite materials  cylindrical shell    non-linear    dynamic response   semi-analytical method
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号