Mechanical analysis and progressive failure prediction for fibre metal laminates using a 3D constitutive model

被引:38
|
作者
Jin, Kai [1 ]
Wang, Hao [2 ]
Tao, Jie [2 ,3 ]
Du, Dandan [4 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Mech & Elect Engn, Nanjing 211106, Jiangsu, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Coll Mat Sci & Technol, Nanjing 211106, Jiangsu, Peoples R China
[3] Jiangsu Collaborat Innovat Ctr Adv Inorgan Funct, Nanjing 211816, Jiangsu, Peoples R China
[4] Beijing Goldwind Sci & Creat Wind Power Equipment, Beijing 100176, Peoples R China
基金
中国国家自然科学基金;
关键词
Fibre metal laminates; 3D constitutive model; Mechanical analysis; Progressive failure; FATIGUE-CRACK GROWTH; SHORT-BEAM-SHEAR; THERMOPLASTIC COMPOSITE; GLARE; BEHAVIOR; FRACTURE; DELAMINATION;
D O I
10.1016/j.compositesa.2019.105490
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Because fibre metal laminates (FMLs) consist of sequentially stacked metal and fibre-reinforced polymer (FRP) laminas, obtaining an accurate description of the mechanical behaviour by a constitutive model can be difficult. In this study, a 3D constitutive model was developed to analyse the mechanical behaviours under tensile and bending conditions. Furthermore, ductile damage of metal layers, failure of FRP layers and interface delamination were predicted by 3D criteria. The influence of the fibre orientation on the mechanical properties was investigated. The stress distribution and progressive failure process of the FMLs were simulated by numerical analysis, the results of which were consistent with the experimental results.
引用
收藏
页数:14
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