Flexural and low velocity impact behaviour of hybrid metal wire mesh/ carbon-fibre reinforced epoxy laminates

dc.authorid0000-0002-3244-1316
dc.contributor.authorCengiz, Abdulkadir
dc.contributor.authorYildirim, Ismail Melih
dc.contributor.authorAvcu, Egemen
dc.date.accessioned2025-05-20T18:59:18Z
dc.date.issued2024
dc.departmentBilecik Şeyh Edebali Üniversitesi
dc.description.abstractRecently, there has been an increasing interest in the development of innovative fibre metal laminates with significantly enhanced flexural strength and impact resistance. The objective of this study is to develop stainlesssteel wire mesh/carbon-fibre reinforced epoxy laminates and examine their flexural and low velocity impact behaviour as a function of steel wire mesh reinforcement. The damage caused by low velocity impact was examined using optical microscopy and micro computed tomography (micro-CT). Steel wire mesh reinforcement increased low velocity impact performance because of its ductility, which dissipates energy across the crosssection and enables the structure to absorb more energy than an unreinforced composite. Scanning electron microscopy images of the composites' cross-sectional microstructure showed the carbon fibres and steel wires' wettability, indicating a strong reinforcement-epoxy matrix interface. Steel wire mesh reduced fragmentation and delamination damage in the impact cone and helped retain composite structural integrity, according to micro-CT data. However, the influence of steel mesh reinforcement on flexural behaviour was insignificant. In conclusion, the developed hybrid metal wire mesh/carbon-fibre reinforced epoxy laminates possess enhanced impact properties, which can make them promising candidates specifically for aerospace and defence applications.
dc.description.sponsorshipKocaeli University Scientific Research Projects Coordination Unit [FBA -2024-3607]
dc.description.sponsorshipThe authors acknowledge the financial support by Kocaeli University Scientific Research Projects Coordination Unit (FBA -2024-3607) .
dc.identifier.doi10.1016/j.coco.2024.101844
dc.identifier.issn2452-2139
dc.identifier.scopus2-s2.0-85184583662
dc.identifier.scopusqualityQ1
dc.identifier.urihttps://doi.org/10.1016/j.coco.2024.101844
dc.identifier.urihttps://hdl.handle.net/11552/8341
dc.identifier.volume46
dc.identifier.wosWOS:001186350100001
dc.identifier.wosqualityQ1
dc.indekslendigikaynakWoS
dc.indekslendigikaynakScopus
dc.indekslendigikaynakWoS - Science Citation Index Expanded
dc.language.isoen
dc.publisherElsevier Sci Ltd
dc.relation.ispartofComposites Communications
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_WOS_20250518
dc.subjectLow velocity impact
dc.subjectCFRP
dc.subjectSteel wire mesh
dc.subjectX-ray CT
dc.subjectDamage mechanisms
dc.titleFlexural and low velocity impact behaviour of hybrid metal wire mesh/ carbon-fibre reinforced epoxy laminates
dc.typeArticle

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