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面内载荷作用下复合材料层合板非线性屈曲
引用本文:龚良贵,侯瑾,李情. 面内载荷作用下复合材料层合板非线性屈曲[J]. 南昌大学学报(工科版), 2011, 33(3): 252-256,260
作者姓名:龚良贵  侯瑾  李情
作者单位:南昌大学建筑工程学院,江西南昌,330031
摘    要:采用广义傅立叶级数法建立了具有弹性约束的复合材料矩形层板在面内载荷作用下的非线性稳定性控制方程组,并简化为矩阵形式。运用广义傅里叶级数法对控制方程组进行求解,得到相应的载荷一中心挠度曲线。计算结果表明:非对称层合板在面内载荷作用下,一般产生的是横向变形,但在一定的铺层顺序、边界条件、受载方式等情况下,也可能发生分叉型屈曲。

关 键 词:复合材料  层合板  非线性屈曲  横向位移

Nonlinear Buckling of Composite Laminated Plates Subjected to In-plane Loading
GONG Liang-gui,HOU Jin,LI Qing. Nonlinear Buckling of Composite Laminated Plates Subjected to In-plane Loading[J]. Journal of Nanchang University(Engineering & Technology Edition), 2011, 33(3): 252-256,260
Authors:GONG Liang-gui  HOU Jin  LI Qing
Affiliation:GONG Liang-gui,HOU Jin,LI Qing(School of Civil Engineering and Architecture,Nanchang University,Nanchang 330031,China)
Abstract:The nonlinear governing equations of rectangular composite laminated plates with edges elastically supported against rotation were established by generalized Fourier series method.The governing equations were simplified in matrix form.The governing equations were solved by using generalized Fourier double series method and the corresponding load-deflection curves were obtained.The results of calculation showed that unsymmetric laminates under loads in plane produced transverse deflection generally,but in so...
Keywords:composite  laminated plates  nonlinear buckling  transverse displacement  
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