Publication:
Enhanced Tensile and Flexural Properties in Carbon Nanotubes and Modified Carbon Nanotubes Added Carbon Fiber-Reinforced Epoxy Resin Thermoset Composites

dc.authorscopusid55486367300
dc.authorscopusid59547364700
dc.authorwosidDemircan, Özgür/Aac-4884-2020
dc.contributor.authorDemircan, O.
dc.contributor.authorIbrahim, M. H. I.
dc.date.accessioned2025-12-11T00:37:35Z
dc.date.issued2025
dc.departmentOndokuz Mayıs Üniversitesien_US
dc.department-temp[Demircan, O.] Ondokuz Mayis Univ, Inst Grad Studies, Dept Nanosci & Nanotechnol, Samsun, Turkiye; [Demircan, O.; Ibrahim, M. H. I.] Ondokuz Mayis Univ, Fac Engn, Met & Mat Engn Dept, Samsun, Turkiyeen_US
dc.description.abstractIn this study, carbon fiber (CF)/epoxy/multi-walled carbon nanotubes (MWCNTs) and CF/epoxy/modified MWCNTs-COOH (weight percentages were 0 and 0.5) were used to fabricate the thermoset composite materials with higher mechanical properties compared to the pristine. The thermoset composites were fabricated using vacuum infusion methods. The addition of MWCNTs on the microstructure of the laminates was studied by using a scanning electron microscope (SEM) and optical microscopy (OM). The samples with MWCNTs-COOH demonstrated an improvement of 26% tensile strength and 43% tensile modulus compared to the samples without MWCNTs. These enhancements were 16% tensile strength and 22% tensile modulus in samples with MWCNTs. The samples with MWCNTs-COOH demonstrated an improvement of 21% flexural strength and 36% flexural modulus compared to the samples without MWCNTs. These enhancements were 9.5% flexural strength and 22% flexural modulus in samples with MWCNTs. Scanning electron and optical microscopic examinations of fractured surfaces showed that the enhancement in the flexural characteristics of MWCNT/epoxy composites was attributed to the better interfacial properties caused by existence of the MWCNTs and MWCNTs-COOH in the epoxy matrix. The results of this research can be applied in advanced manufacturing of composite materials in Industry 4.0 in aerospace (such as parts of fuselage panels, skins and spars).en_US
dc.description.sponsorshipResearch fund of Ondokuz Mayimath;s University [PYO.TIP.1908.20.001, PYO.MUH.1901.18.008]en_US
dc.description.sponsorshipThe authors would like to thank to the Research fund of Ondokuz May & imath;s University (Project Numbers: PYO.TIP.1908.20.001 and PYO.MUH.1901.18.008).en_US
dc.description.woscitationindexScience Citation Index Expanded
dc.identifier.doi10.1007/s11665-025-10664-1
dc.identifier.endpage18798en_US
dc.identifier.issn1059-9495
dc.identifier.issn1544-1024
dc.identifier.issue17en_US
dc.identifier.scopus2-s2.0-85217213331
dc.identifier.scopusqualityQ3
dc.identifier.startpage18787en_US
dc.identifier.urihttps://doi.org/10.1007/s11665-025-10664-1
dc.identifier.urihttps://hdl.handle.net/20.500.12712/38002
dc.identifier.volume34en_US
dc.identifier.wosWOS:001401156800001
dc.identifier.wosqualityQ3
dc.language.isoenen_US
dc.publisherSpringeren_US
dc.relation.ispartofJournal of Materials Engineering and Performanceen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectCarbon Nanotubes and Modified Carbon Nanotubesen_US
dc.subjectCFRPen_US
dc.subjectIndustry 4.0en_US
dc.subjectTensile and Bending Propertiesen_US
dc.subjectVacuum Infusionen_US
dc.titleEnhanced Tensile and Flexural Properties in Carbon Nanotubes and Modified Carbon Nanotubes Added Carbon Fiber-Reinforced Epoxy Resin Thermoset Compositesen_US
dc.typeArticleen_US
dspace.entity.typePublication

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