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Displacement rate effects on mixed-mode I/II delamination of laminated carbon/epoxy composites

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dc.contributor.author Kean Ong Low
dc.contributor.author Mahzan Johar
dc.contributor.author Aun Naa Sung
dc.contributor.author Mohd Nazri Mohd Nasir
dc.contributor.author Seyed Saeid Rahimian Koloor
dc.contributor.author Michal Petru
dc.contributor.author Haris Ahmad Israr
dc.contributor.author King Jye Wong
dc.contributor.author (UniKL MITEC)
dc.date.accessioned 2023-07-05T03:04:46Z
dc.date.available 2023-07-05T03:04:46Z
dc.date.issued 2023-07-05
dc.identifier.uri http://hdl.handle.net/123456789/28043
dc.description This article is index by Scopus. en_US
dc.description.abstract Mixed-mode delamination is one of the common failures of composites which has not been studied under low-impact loading. This paper studies the influence of displacement rate on mixed-mode I/II delamination of unidirectional carbon/epoxy composites. Single leg bending test is performed at displacement rates of 1, 10, 100, and 500 mm/min. Experimental results reveal that the mixed-mode I/II fracture toughness is invariant with the displacement rate. In addition, scanning electron micrographs shows that shear cusps are more obvious at 1, 10, and 100 mm/min. At 500 mm/min, significant matrix debris is noticed. Furthermore, the proposed three-dimensional rate-dependent fracture criterion is found to well predict the fracture toughness. Numerical simulation using cohesive zone model suggests that the lower numerical peak load is due to lower damage dissipated energy. In addition, the theoretical and numerical traction-separation responses show significant differences, which is also reflected in the numerical phase angle. This implies that the local mixed-mode ratio is not constant throughout the simulation process. en_US
dc.subject Carbon/epoxy composite en_US
dc.subject Cohesive zone modelling en_US
dc.subject Fractography en_US
dc.subject Mixed-mode delamination en_US
dc.subject Rate dependence en_US
dc.title Displacement rate effects on mixed-mode I/II delamination of laminated carbon/epoxy composites en_US


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