Print Email Facebook Twitter Fatigue delamination behavior in composite laminates at different stress ratios and temperatures Title Fatigue delamination behavior in composite laminates at different stress ratios and temperatures Author Yao, Liaojun (Harbin Institute of Technology) Chuai, Mingyue (Harbin Institute of Technology) Liu, J. (Harbin Institute of Technology) Guo, Licheng (Harbin Institute of Technology) Chen, Xiangming (Aircraft Strength Research Institute) Alderliesten, R.C. (TU Delft Structural Integrity & Composites; Structural Integrity and Composite Group) Beyens, M. (Student TU Delft) Date 2023 Abstract This study provides an investigation on mode I fatigue delamination growth (FDG) with fibre bridging at different R-ratios and temperatures in carbon-fibre reinforced polymer composites. FDG experiments were first conducted at different temperatures of R-ratios 0.1 and 0.5 via unidirectional double cantilever beam (DCB) specimens. A fatigue model, employing both the strain energy release rate (SERR) range and the maximum SERR around crack front as similitude parameter, was proposed to interpret FDG behavior. The use of this model can collapse FDG data with fibre bridging at different R-ratios into one master curve, obeying well with the similitude principles. Accordingly, it was found that FDG can accelerate with elevated temperature, but decrease at sub-zero temperature. Furthermore, there are strong correlations between the fatigue model parameters and temperature using this model in FDG interpretations. Taking these correlations into account can extend the model to accurately predict FDG behavior of other temperatures. Fractographic examinations demonstrated that temperature has effects on the FDG damage mechanisms. Both fibre/matrix interfacial debonding and matrix brittle failure were observed in FDG of −40℃. Fibre/matrix interfacial debonding becomes the dominant failure in FDG of RT and 80℃. No obvious difference on the fracture morphology was identified for FDG at different R-ratios of a given temperature. Subject Composite laminatesFatigue delaminationFibre bridgingR-ratioTemperature To reference this document use: http://resolver.tudelft.nl/uuid:4d82e915-6953-4ba1-9266-3dada5a3b692 DOI https://doi.org/10.1016/j.ijfatigue.2023.107830 Embargo date 2024-01-08 ISSN 0142-1123 Source International Journal of Fatigue, 175 Bibliographical note Green Open Access added to TU Delft Institutional Repository ‘You share, we take care!’ – Taverne project https://www.openaccess.nl/en/you-share-we-take-care Otherwise as indicated in the copyright section: the publisher is the copyright holder of this work and the author uses the Dutch legislation to make this work public. Part of collection Institutional Repository Document type journal article Rights © 2023 Liaojun Yao, Mingyue Chuai, J. Liu, Licheng Guo, Xiangming Chen, R.C. Alderliesten, M. Beyens Files PDF 1_s2.0_S0142112323003316_main.pdf 8.22 MB Close viewer /islandora/object/uuid:4d82e915-6953-4ba1-9266-3dada5a3b692/datastream/OBJ/view