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dc.contributor.authorSeyhan, Abdullah Tuğrul
dc.contributor.authorSun, Z.
dc.contributor.authorDeitzel, J.
dc.contributor.authorTanoğlu, M.
dc.contributor.authorHeider, D.
dc.date.accessioned2019-10-22T16:58:47Z
dc.date.available2019-10-22T16:58:47Z
dc.date.issued2009
dc.identifier.issn0254-0584
dc.identifier.issn1879-3312
dc.identifier.urihttps://dx.doi.org/10.1016/j.matchemphys.2009.07.045
dc.identifier.urihttps://hdl.handle.net/11421/21615
dc.descriptionWOS: 000271556000042en_US
dc.description.abstractIn this study, the cure kinetics of Cycom 977-20. an aerospace grade toughened epoxy resin, and its suspensions containing various amounts (1, 3 and 5 wt.%) of vapor grown carbon nanofibers (VGCNFs) with and without chemical treatment were monitored via dynamic and isothermal dynamic scanning calorimetry (DSC) measurements. For this purpose, VGCNFs were first oxidized in nitric acid and then functionalized with 3-glycidoxypropyltrimethoxy silane (GPTMS) coupling agent. Fourier transform infrared (FTIR) spectroscopy was subsequently used to verify the chemical functional groups grafted onto the surfaces of VGCNFs. Sonication technique was conducted to facilitate proper dispersion of as-received, acid treated and silanized VGCNFs within epoxy resin. Dynamic DSC measurements showed that silanized VGCNF modified resin suspensions exhibited higher heat of cure compared to those with as-received VGCNFs. Experimentally obtained isothermal DSC data was then con elated with Kamal phenomenological model. Based on the model predictions, it was found that silanized VGCNFs; maximized the cure reaction rates at the very initial stage of the reaction. Accordingly, an optimized curing cycle was applied to harden resin suspensions. Fracture testing was then carried out on the cured samples in order to relate the curing behavior of VGCNF modified resin suspensions to mechanical response of their resulting nanocomposites With addition of 1 wt % of silanized VGCNFs, the fracture toughness value of neat epoxy was found to be improved by 12%. SEM was further employed to examine the fracture surfaces of the samplesen_US
dc.description.sponsorshipOffice of Naval Research [N00014-02-1-0811]; Advanced Materials Intelligent Processing Center at the Center for Composite Materials; University of Delawareen_US
dc.description.sponsorshipThis work was supported by the Office of Naval Research through the project (N00014-02-1-0811)Advanced Materials Intelligent Processing Center at the Center for Composite Materials (CCM), University of Delaware. The authors also wish to thank Abdel Abusafieh and Rick Price from Cytec Industries Inc., for providing the toughened epoxy resin.en_US
dc.language.isoengen_US
dc.publisherElsevier Science Saen_US
dc.relation.isversionof10.1016/j.matchemphys.2009.07.045en_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.subjectPolymersen_US
dc.subjectNanostructuresen_US
dc.subjectDynamic Scanning Calorimetry (Dsc)en_US
dc.subjectFracture And Toughnessen_US
dc.titleCure kinetics of vapor grown carbon nanofiber (VGCNF) modified epoxy resin suspensions and fracture toughness of their resulting nanocompositesen_US
dc.typearticleen_US
dc.relation.journalMaterials Chemistry and Physicsen_US
dc.contributor.departmentAnadolu Üniversitesi, Mühendislik Fakültesi, Malzeme Bilimi ve Mühendisliği Bölümüen_US
dc.identifier.volume118en_US
dc.identifier.issue1en_US
dc.identifier.startpage234en_US
dc.identifier.endpage242en_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US


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