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

•Iosipescu method is extended to explore interlaminar shear fatigue behavior of CFRP.•Two stress ratios and four stress levels yield S-N and stiffness degradation curves.•A significant three-stage cumulative damage evolution characteristic is captured.•Fatigue-induced debonding and delamination are...

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Bibliographic Details
Published in:International journal of fatigue 2024-01, Vol.178, p.108020, Article 108020
Main Authors: Lei, Zuxiang, Luo, Gan, Sun, Weikang, Dong, Yawei, Tan, Zhifei, Wan, Yun, Yin, Binbin
Format: Article
Language:English
Subjects:
Carbon fiber reinforced composite
Failure mechanism
Interlaminar shear fatigue
Iosipescu method
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Summary:•Iosipescu method is extended to explore interlaminar shear fatigue behavior of CFRP.•Two stress ratios and four stress levels yield S-N and stiffness degradation curves.•A significant three-stage cumulative damage evolution characteristic is captured.•Fatigue-induced debonding and delamination are analyzed via microscopic observation. 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 (τ) and interlaminar shear modulus (G13) in the static tests, this work conducted interlaminar 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 cumulative damage evolution characteristic is 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.
ISSN:0142-1123
DOI:10.1016/j.ijfatigue.2023.108020