An Experimental and Numerical Determination on Low-Velocity Impact Response of Hybrid Composite Laminate

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dc.authoridEker Gumus, Beril/0000-0002-4185-4470
dc.contributor.authorErbayrak, Engin
dc.contributor.authorYuncuoglu, Ercument Ugur
dc.contributor.authorKahraman, Yusuf
dc.contributor.authorGumus, Beril Eker
dc.date.accessioned2024-10-04T18:48:12Z
dc.date.available2024-10-04T18:48:12Z
dc.date.issued2021
dc.departmentBayburt Üniversitesien_US
dc.description.abstractIn this study, experimental and numerical investigations were carried out in order to determine the mechanical properties and impact response of hybrid composite laminate. The hybrid composite laminate was formed from plain woven carbon fiber reinforced epoxy (CFRE) and plain woven glass fiber reinforced epoxy (GFRE) fiber using VARTM (vacuum-assisted resin transfer molding) process. The mechanical properties of the hybrid composites were determined using tensile test device with a 1 mm/min loading rate at room temperature. In addition, hybrid composites were subjected to low-velocity impact test under different impact energy levels (10, 20, 30, 40 J) for determining the impact response. Moreover, mechanical properties and impact responses of CFRE and GFRE laminates were also determined to compare to those of hybrid composite (HCGFRE). Microstructure analysis was performed to investigate the damage surfaces of the fiber and matrix in the composite material subjected to impact and tensile forces. In numerical analyses, composite damage model (Mat 54) was utilized in LS-DYNA(R)explicit finite element program to simulate the impact behavior of CFRE, GFRE and HCGFRE laminates. Consequently, the tensile test results showed that hybrid composite laminate behaved more ductile than carbon composite laminate and it exhibited more brittle behavior than glass composite laminate. Also, it was determined that absorbed energy and impact load capacity of HCGFRE composite laminate are between absorbed energy and impact load capacity of CFRE and GFRE composite laminate. It was determined that numerical results indicate a similar tendency with the experimental results.en_US
dc.identifier.doi10.1007/s40997-020-00402-4
dc.identifier.endpage681en_US
dc.identifier.issn2228-6187
dc.identifier.issn2364-1835
dc.identifier.issue3en_US
dc.identifier.scopus2-s2.0-85092726056en_US
dc.identifier.scopusqualityQ2en_US
dc.identifier.startpage665en_US
dc.identifier.urihttps://doi.org/10.1007/s40997-020-00402-4
dc.identifier.urihttp://hdl.handle.net/20.500.12403/2960
dc.identifier.volume45en_US
dc.identifier.wosWOS:000579688000001en_US
dc.identifier.wosqualityQ3en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherSpringeren_US
dc.relation.ispartofIranian Journal of Science and Technology-Transactions of Mechanical Engineeringen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectHybrid compositeen_US
dc.subjectLow-velocity impacten_US
dc.subjectMechanical propertiesen_US
dc.subjectFinite element analysesen_US
dc.subjectVacuum-assisted resin transfer moldingen_US
dc.titleAn Experimental and Numerical Determination on Low-Velocity Impact Response of Hybrid Composite Laminateen_US
dc.typeArticleen_US

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