玻璃钢/复合材料Issue(5)：34-40,7.
复合材料帽型加筋板界面应力与失效模拟
INTERFACIAL STRESSES AND FAILURE SIMULATION OF COMPOSITE HAT-STIFFENED PANEL
摘要
Abstract
Based on CZM (Cohesive Zone Model),FEM model is built up to study the interfacial stresses and debonding failure of the composite hat-stiffened panel subjected to four-point bending.In the present model,the debonding failure of the adhesive layer between the skin and stiffener is considered by adding interface elements between the solid elements.The results indicate that:adhesive debonding is the main failure pattern of composite hatstiffened panel,shear stress has a major effect on the debonding of bondline,and the failure of the adhesive layer can largely decrease the load-carrying capacity of the structure and lead to more serious damage.关键词
复合材料/帽型加筋板/内聚力模型/有限元/界面应力Key words
composites/hat-stiffened panel/cohesive zone model/finite element/interfacial stresses分类
通用工业技术引用本文复制引用
黄凌凯,朱礼宝,章向明,王安稳..复合材料帽型加筋板界面应力与失效模拟[J].玻璃钢/复合材料,2017,(5):34-40,7.基金项目
国家自然科学基金项目(51479206) （51479206）
