The effect of lamina configuration on low-velocity impact behaviour for glass fiber/rubber curved composites

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dc.authoridbozkurt, ilyas/0000-0001-7850-2308
dc.authoridalbayrak, mustafa/0000-0002-2913-6652
dc.authorwosidbozkurt, ilyas/HKE-1178-2023
dc.authorwosidKaman, Mete Onur/V-9306-2018
dc.authorwosidALBAYRAK, Mustafa/AFB-4566-2022
dc.contributor.authorAlbayrak, Mustafa
dc.contributor.authorKaman, Mete Onur
dc.contributor.authorBozkurt, Ilyas
dc.date.accessioned2024-08-04T20:53:33Z
dc.date.available2024-08-04T20:53:33Z
dc.date.issued2023
dc.departmentİnönü Üniversitesien_US
dc.description.abstractThe aim of this study is to produce curved sandwich composites with different arrays by adding Ethylene Propylene Diene Monomer (EPDM) rubber interlayers between glass fiber woven fabrics and to investigate their behaviours under low-velocity impact. For this purpose, sandwich plates were produced through the vacuum infusion method by using glass fiber and rubber layers on the steel mold manufactured in curved form. Impact tests were applied on the plates and the effect of the stacking sequence for glass fibers/rubber layer on the impact energy absorption was examined. The energy absorption property of the composites was improved by a maximum of 45% with a layer epdm used in the midplane of the composite. Also, when rubber layers were used on the outermost surface of the composites, the damage area reduced by 14%. In the numerical part, the tests were modelled using LS-DYNA finite element packaged programme and the Hashin failure criterion-based material model was used in order to view any damages on the composite structure after the tests. The agreement between numerical and experimental results was obtained with a maximum error of 19%en_US
dc.description.sponsorshipFirat University Scientific Research Coordination Unit [MF20.10]en_US
dc.description.sponsorshipThe author(s) disclosed receipt of the following financial support for the research, authorship, and/or publication of this article: This work was supported by the Firat University Scientific Research Coordination Unit, which supported this study with the project number: MF20.10.en_US
dc.identifier.doi10.1177/00219983231164950
dc.identifier.endpage1907en_US
dc.identifier.issn0021-9983
dc.identifier.issn1530-793X
dc.identifier.issue11en_US
dc.identifier.scopus2-s2.0-85151072473en_US
dc.identifier.scopusqualityQ2en_US
dc.identifier.startpage1875en_US
dc.identifier.urihttps://doi.org/10.1177/00219983231164950
dc.identifier.urihttps://hdl.handle.net/11616/101255
dc.identifier.volume57en_US
dc.identifier.wosWOS:000956544800001en_US
dc.identifier.wosqualityQ3en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherSage Publications Ltden_US
dc.relation.ispartofJournal of Composite Materialsen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectCurved compositesen_US
dc.subjectrubber layeren_US
dc.subjectprogressive failure analysisen_US
dc.subjectlow-velocity impacten_US
dc.titleThe effect of lamina configuration on low-velocity impact behaviour for glass fiber/rubber curved compositesen_US
dc.typeArticleen_US

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