Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.13091/999
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dc.contributor.authorMetin, Fatih-
dc.contributor.authorAvcı, Ahmet-
dc.date.accessioned2021-12-13T10:32:18Z-
dc.date.available2021-12-13T10:32:18Z-
dc.date.issued2021-
dc.identifier.issn0263-8223-
dc.identifier.issn1879-1085-
dc.identifier.urihttps://doi.org/10.1016/j.compstruct.2021.114085-
dc.identifier.urihttps://hdl.handle.net/20.500.13091/999-
dc.description.abstractEight-ply glass/epoxy composites interleaved by electrospun Polysulfone (PSF) nanofibers were manufactured by vacuum-assisted hand lay-up method. The effect of nanofibrous interlaminar layers on the mechanical performance of laminated composites was investigated under both in-plane quasi-static and out-of-plane lowvelocity impact (LVI) test conditions. Low-velocity impact responses of reference and nanofiber interleaved composite laminates were modeled by LS-Dyna finite element (FE) code for numerical simulations. The results of the quasi-static mechanical tests show that PSF nanofiber interleaving increases the tensile and compressive strength by 10.5% and 25.5%, respectively. PSF nanofibers played an important role in improving the impact damage resistance of composite laminates with increasing impact energy levels. The low-velocity impact tests results indicated that PSF nanofibers decreased the fiber breakage area at 20 J and 30 J energy levels by about 26% and 28%, respectively. Besides, PSF nanofiber interleaving improved damage threshold load values by 4.8%, 15.2%, and 23% at 10 J, 20 J, and 30 J energy levels, respectively. Experimental and FE simulation results were comparatively presented in terms of force-time, force-deflection, and energy-time curves. A good agreement was achieved between experimental and simulation results.en_US
dc.description.sponsorshipScientific and Technological Research Council of Turkey (TUBTAK)Turkiye Bilimsel ve Teknolojik Arastirma Kurumu (TUBITAK) [215M777]en_US
dc.description.sponsorshipThe authors would like to thank The Scientific and Technological Research Council of Turkey (TUBTAK) (Project No: 215M777) for their financial support.en_US
dc.language.isoenen_US
dc.publisherELSEVIER SCI LTDen_US
dc.relation.ispartofCOMPOSITE STRUCTURESen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectLow-Velocity Impacten_US
dc.subjectFinite Element Analysisen_US
dc.subjectComposite Laminatesen_US
dc.subjectNanofibersen_US
dc.subjectPolysulfoneen_US
dc.subjectInterleavingen_US
dc.subjectLow-Velocity Impacten_US
dc.subjectDelaminationen_US
dc.subjectStrengthen_US
dc.subjectCriteriaen_US
dc.subjectDamagesen_US
dc.subjectPhaseen_US
dc.titleIn-plane quasi-static and out-of-plane dynamic behavior of nanofiber interleaved glass/epoxy composites and finite element simulationen_US
dc.typeArticleen_US
dc.identifier.doi10.1016/j.compstruct.2021.114085-
dc.identifier.scopus2-s2.0-85107649364en_US
dc.departmentFakülteler, Mühendislik ve Doğa Bilimleri Fakültesi, Metalurji ve Malzeme Mühendisliği Bölümüen_US
dc.identifier.volume270en_US
dc.identifier.wosWOS:000662842100004en_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.authorscopusid57202228561-
dc.authorscopusid57224695830-
dc.identifier.scopusqualityQ1-
item.languageiso639-1en-
item.fulltextWith Fulltext-
item.cerifentitytypePublications-
item.openairetypeArticle-
item.grantfulltextembargo_20300101-
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
Appears in Collections:Mühendislik ve Doğa Bilimleri Fakültesi Koleksiyonu
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collections
WoS İndeksli Yayınlar Koleksiyonu / WoS Indexed Publications Collections
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