Analysis of Stochastic Matrix Crack Evolution in CFRP Cross-Ply Laminates under Fatigue Loading

Journal Article (2023)
Author(s)

X. Li (TU Delft - Structural Integrity & Composites, Center of Excellence in Artificial Intelligence for Structures)

R Benedictus (TU Delft - Structural Integrity & Composites)

Dimitrios Zarouchas (Center of Excellence in Artificial Intelligence for Structures, TU Delft - Structural Integrity & Composites)

Research Group
Structural Integrity & Composites
Copyright
© 2023 X. Li, R. Benedictus, D. Zarouchas
DOI related publication
https://doi.org/10.1016/j.engfailanal.2023.107277
More Info
expand_more
Publication Year
2023
Language
English
Copyright
© 2023 X. Li, R. Benedictus, D. Zarouchas
Research Group
Structural Integrity & Composites
Volume number
150
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

The present work aims at understanding the stochastic matrix crack evolution in CFRP cross-ply laminates under tension–tension fatigue loading. An experimental campaign was carried out on twenty-three specimens at different stress levels, while two optical techniques were used for the in-situ monitoring of the accumulation of transverse matrix cracks. The results showed a significant scatter in crack evolution among specimens. This stochastic behaviour was further investigated using image analysis and numerical modelling. It was found that transverse matrix cracks can be classified into the independent and dependent cracks based on a critical crack spacing. Furthermore, the severity of interaction among cracks was quantified by introducing a dependent crack ratio. Finally, a strength-based probabilistic model was proposed to describe the scattering regime of the crack evolution. The agreement between model and test results indicates that local strength variations of 90 plies are the dominant scattering source governing the initial fatigue resistance to cracking and determining the accumulation of transverse matrix cracks among specimens. These results may provide a new insight into the stochastic nature of matrix cracking in composite laminates and aid in the design of fatigue resistance properties.