碳纤维增强环氧树脂复合材料加筋板的压缩屈曲特性  

Compressive Buckling Property of Carbon Fiber Reinforced Epoxy Resin Composite Stiffened Panel

作　　者：张浩宇[1] 何宇廷[1] 冯宇[1] 谭翔飞[1] 邵青[1] 尹翔 

机构地区：[1]空军工程大学航空航天工程学院,西安710038 [2]陆航驻203所军事代表室,西安710038

出　　处：《机械工程材料》2015年第12期59-62,共4页Materials For Mechanical Engineering

基　　金：国家自然科学基金资助项目(51475470)

摘　　要：分别应用工程算法和有限元软件ANSYS对碳纤维增强环氧树脂复合材料加筋板的压缩稳定性进行了分析,得到了加筋板的临界失稳屈曲载荷和屈曲模态;同时对复合材料加筋板进行了压缩稳定性试验,并与计算结果进行了对比验证。结果表明:碳纤维增强环氧树脂复合材料加筋板具有后屈曲承载能力,其压缩破坏形式主要为筋条的脱胶、断裂和蒙皮的撕裂;工程算法结果、有限元计算结果与试验得到的临界屈曲载荷误差分别为13.8%和-15.5%,结果较吻合,证明了工程算法的正确性和有限元模拟方法的合理性。The compression stability of carbon fiber reinforced epoxy resin composite stiffened panel was analyzed by the engineering method and finite element model（FEM）respectively,and the critical buckling load and buckling mode of the stiffened panel were obtained.The experiments on the compression stability of the composite stiffened panel were conducted and the experimental results were compared with the calculated results.The results show that the composite stiffened panel had a certain post-buckling carrying capacity,and the failure mode consisted of the adhesive failure and fracture of stiffener and the tearing of skin.The error between the critical buckling load calculated by the engineering method and FEM method and that of experiment was 13.8% and-15.5%respectively.The results agreed well,indicating the accuracy of the engineering method and the reasonableness of the finite element model.

关 键 词：复合材料加筋板 屈曲特性 压缩稳定性 有限元模型 工程算法 

分 类 号：V258[一般工业技术—材料科学与工程]