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层合中厚非圆截面柱壳非线性动力稳定性分析
引用本文:傅衣铭,欧耀辉,高正强.层合中厚非圆截面柱壳非线性动力稳定性分析[J].湖南大学学报(自然科学版),2007,34(6):54-58.
作者姓名:傅衣铭  欧耀辉  高正强
作者单位:湖南大学,力学与航空航天学院,湖南,长沙,410082
基金项目:国家自然科学基金资助项目(10572049)
摘    要:基于Timoshenko-Midlin假设及Hamilton变分原理,建立了层合中厚非圆柱壳的非线性运动控制方程,采用伽辽金技术,得到仅含时间参数的Mathieu型方程,然后应用增量谐波平衡法进行求解.数值计算中,以两端简支L曲线截面层合中厚柱壳为例,讨论了截面形状参数、几何非线性和横向剪切效应等因素对层合中厚非圆截面柱壳非线性动力稳定性的影响.结果表明:这些因素对层合L曲线截面中厚柱壳的非线性主要动力不稳定区域有较大影响.

关 键 词:层合非圆截面柱壳  横向剪切变形  非线性动力稳定性
文章编号:1000-2472(2007)06-0054-05
修稿时间:2006-11-07

Analysis of Nonlinear Dynamic Stability for Laminated Non-Circular Cross-section Calumn Thick Shells
FU Yi-ming,OU Yao-hui,GAO Zheng-qiang.Analysis of Nonlinear Dynamic Stability for Laminated Non-Circular Cross-section Calumn Thick Shells[J].Journal of Hunan University(Naturnal Science),2007,34(6):54-58.
Authors:FU Yi-ming  OU Yao-hui  GAO Zheng-qiang
Institution:College of Mechanics and Aerospace, Hunan Univ, Changsha, Hunan 410082, China
Abstract:Based on the Timoshenko-Mindlin hypothesis and the Hamilton Principle, a set of governing equations of motion for the laminated non-circular cylindrical thick shells were founded.Using the Galerkin procedure,the Mathieu equation only with time variable was obtained,and this equation was solved by the method of increase harmonic balance.In numerical calculation,the laminated L-curve section cylindrical thick shells with both ends simply supported were investigated,and the effects of sectional shape,geometrically nonlinear factors and transverse shear on the nonlinear dynamic stability of laminated non-circular cylindrical shells were discussed.The results indicate these factors have a tremendous influence on the nonlinear dynamic stability of laminated non-circular cylindrical shells.
Keywords:laminated non-circular cylindrical shells  transverse shear deformation  nonlinear dynamic stability
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