Different effects of interfacial properties on the tensile and compressive damage mechanisms of 3D woven composites: Multiscale damage model and numerical comparative study

被引:9
作者
Zheng, Tao [1 ]
Huang, Jinzhao [1 ]
Huang, Kai [1 ]
Yu, Hongjun [1 ]
Hong, Changqing [1 ]
Guo, Licheng [1 ]
机构
[1] Harbin Inst Technol, Dept Astronaut Sci & Mech, Harbin 150001, Peoples R China
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
3D woven composites; Interface debonding; Multiscale damage model; Damage mechanism; Numerical comparative study; FIBER-REINFORCED COMPOSITES; PROGRESSIVE DAMAGE; INTERLAMINAR FRACTURE; FAILURE CRITERIA; PART II; BEHAVIOR; MICROMECHANICS; DISTRIBUTIONS;
D O I
10.1016/j.engfracmech.2023.109741
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A multiscale damage model is proposed based on a micro-mesoscale bridging model and a multiscale kinking model, which can predict the damage development processes of 3D woven composites (3DWCs) under different loading conditions using only few material parameters. At the microscale, the various mesoscopic damage modes of yarns, including tensile fiber breakage, compressive fiber kinking and transverse inter-fiber crack, can be simply divided into matrix-and fiber-dominated damage. Using this multiscale damage model, a numerical comparative study is conducted to investigate the effect of interfacial properties on the mechanical performances and damage mechanism of 3DWCs. The numerical results indicate that the interfacial properties exhibit different effects on the tensile and compressive strengths and damage mechanisms of 3DWCs. The interaction of different damage modes controls the overall trend of the tensile strength of 3DWCs. There is an optimum point for the tensile strength of 3DWCs at different interfacial fracture toughness. Beyond the optimum point, the tensile strength of 3DWCs is negatively correlated with interfacial properties. Unlike the tensile loading case, the better the interfacial properties, the later fiber kinking occurs, resulting in higher compressive strength of 3DWCs.
引用
收藏
页数:17
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