含分层损伤复合材料加筋层合板的分层扩展研究

Numerical Analysis of Delamintation Growth for Stiffened Composite Laminated Plates

建立了复合材料加筋结构的后屈曲和分层损伤扩展行为的数值模拟方法· 基于Mindlin一阶剪切理论和von＿K rm n大挠度理论的层合板和层合梁单元,提出了含分层损伤复合材料加筋层合板分层扩展行为的有限元分析方法;利用虚裂纹闭合技术计算分层前缘的总能量释放率,并采用总能量释放率准则分层扩展判据,结合自适应网格移动技术,对在压缩载荷作用下的具有不同加筋形式,不同初始分层面积和形状的加筋板结构分层扩展行为进行了数值模拟研究,在分析中还考虑了加筋刚度、位置和分布,分层形状和大小。

A study of postbuckling and delamination propagation behavior in delaminated stiffened composite plates is presented. A methodology is proposed for simulating the multi-failure responses, such as initial and postbuckling, delamination onset and propagation, etc. A finite element analysis was conducted on the basis of the Mindlin first order shear effect theory and the von-Krmn non^linear deformation assumption. The total energy release rate used as the criteria of delamination growth was estimated with virtual crack closure technique (VCCT). A self-adaptive grid moving technology was adopted to model the delamination growth process. Moreover, the contact effect along delamination front was also considered during the numerical simulation process. By some numerical examples, the influence of distribution and location of stiffener, configuration and size of the delamination, boundary condition and contact effect upon the delamination growth behavior of the stiffened composite plates were investigated. The method and numerical conclusion provided should be of great value to engineers dealing with composite structures.