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Model Investigation on Composite Failure Prediction of π-Joint Structures

查看全文 作  者:Zhao [1]Libin;Qin [1]Tianliang;[1]Huanghai;Liang [2]Xianzhu;Chang [2]Haifeng;Cao [2]Zhenghua 高影响力作者 机构地区:[1]Beijing University of Aeronautics and Astronautics, Beijing 100083, China;[2]China Beijing Aeronautical Manufacturing Technology Research Institute, Beijing 100024, China高影响力机构 出  处:《稀有金属材料与工程》索引2009年第38卷第A03期,共4页高影响力期刊 摘  要:This paper was concerned with the tensile mechanics behavior of the composite π-joint under static tensile loading. The numerical strength analysis methodology was presented containing the basis assumption for the analysis, the material modeling, and the selected element type. It was assumed that the composite ply had transverse isotropic material properties and the adhesive had linear elastic properties. With the goal of the strength analysis to determine the onset of the damage initiation and the ultimate failure load, two stiffness degradation models were discussed and a modified maximum stress failure criteria was presented. To verify the numerical model, a pull-off test scheme was performed and the experimental data of five specimens were given. The experimental results indicate that the damage initiation location and the failure load were consistent with numerical predictions and verified the feasibility of the numerical model. 关 键 词:复合材料 胶粘剂 拉伸力学 复合层
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