On the residual stresses and fracture toughness of glass/carbon epoxy composites

Umarfarooq, M. A. and Gouda, P. S. Shivakumar and Banapurmath, N. R. and Kittur, Mohammed Ibrahim and Khan, Tabrej and Badruddin, Irfan Anjum and Kamangar, Sarfaraz and Hussien, Mohamed (2022) On the residual stresses and fracture toughness of glass/carbon epoxy composites. Materials, 15 (20). ISSN 1996-1944, DOI https://doi.org/10.3390/ma15207135.

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Abstract

The resistance to delamination in polymer composite depends on their constituents, manufacturing process, environmental factors, specimen geometry, and loading conditions. The manufacturing of laminated composites is usually carried out at an elevated temperature, which induces thermal stresses in composites mainly due to a mismatch in the coefficient of thermal expansion (CTE) of fiber and matrix. This work aims to investigate the effect of these process-induced stresses on mode-I interlaminar fracture toughness (G(I)) of Glass-Carbon-Epoxy (GCE) and Glass-Epoxy (GE) composites. These composites are prepared using a manual layup technique and cured under room temperature, followed by post-curing using different curing conditions. Double cantilever beam (DCB) specimens were used to determine G(I) experimentally. The slitting technique was used to estimate residual stresses (longitudinal and transverse direction of crack growth) inherited in cured composites and the impact of these stresses on G(I) was investigated. Delaminated surfaces of composites were examined using a scanning electron microscopy (SEM) to investigate the effect of post-curing on the mode-I failure mechanism. It was found that G(I) of both GE and GEC composites are sensitive to the state of residual stress in the laminas. The increase in the G(I) of laminates can also be attributed to an increase in matrix deformation and fiber-matrix interfacial bond with the increase in post-curing temperature.

Item Type: Article
Funders: Large Groups Project, King Khalid University [RGP.2/1/43]
Uncontrolled Keywords: Interlaminar fracture toughness; Hybrid composites; Residual stresses; Slitting method; SEM
Subjects: T Technology > TA Engineering (General). Civil engineering (General)
Depositing User: Ms. Juhaida Abd Rahim
Date Deposited: 26 Sep 2023 00:56
Last Modified: 26 Sep 2023 00:56
URI: http://eprints.um.edu.my/id/eprint/40873

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