Exploring the Iosipescu method to investigate interlaminar shear fatigue behavior and failure mechanisms of carbon fiber reinforced composites

被引:7
|
作者
Lei, Zuxiang [1 ,2 ,3 ]
Luo, Gan [1 ]
Sun, Weikang [4 ]
Dong, Yawei [5 ]
Tan, Zhifei [6 ]
Wan, Yun [1 ]
Yin, Binbin [4 ,6 ]
机构
[1] East China Jiaotong Univ, Sch Civil Engn & Architecture, Nanchang 330013, Peoples R China
[2] East China Jiaotong Univ, State Key Lab Performance Monitoring & Protecting, Nanchang 330013, Peoples R China
[3] Engn Res & Dev Ctr Underground Technol Jiangxi Pro, Nanchang 330013, Peoples R China
[4] City Univ Hong Kong, Dept Architecture & Civil Engn, Hong Kong, Peoples R China
[5] Yancheng Inst Technol, Coll Civil Engn, Yancheng 224051, Jiangsu, Peoples R China
[6] Hong Kong Polytech Univ, Dept Civil & Environm Engn, Hong Kong, Peoples R China
基金
中国国家自然科学基金;
关键词
Carbon fiber reinforced composite; Iosipescu method; Interlaminar shear fatigue; Failure mechanism; TENSION-COMPRESSION FATIGUE; DAMAGE PROGRESSION; STRENGTH; TEMPERATURE; FIELD; LIFE;
D O I
10.1016/j.ijfatigue.2023.108020
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Iosipescu method, commonly adopted to determine the static shear properties of composite material, is extended to analyze the shear fatigue properties of carbon fiber reinforced epoxy composites. Following the results of the ultimate shear strength (tau) and interlaminar shear modulus (G13) in the static tests, this work conducted inter-laminar shear fatigue tests with two stress ratios and four stress levels to obtain the S-N and stiffness degradation curves. The S-N curves of the stress level versus logarithmic fatigue life exhibit a good linear relationship, and the specimens display a better fatigue performance at the stress ratio of 0.1 than-1. A significant three-stage cu-mulative damage evolution characteristic was found in the fatigue stiffness degradation process. In addition, the damage evolution, dominated by the propagation of matrix microcracks along the fiber direction inside the material, that is, debonding and delamination of the interface, was captured and analyzed via microscopic observation of the damaged zone on the specimen surface. Understanding the revealed processes of shear fatigue failure is crucial for ensuring the safe utilization of composite structures.
引用
收藏
页数:11
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