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dc.contributor.authorCrupi V.
dc.contributor.authorKara E.
dc.contributor.authorEpasto G.
dc.contributor.authorGuglielmino E.
dc.contributor.authorAykul H.
dc.date.accessioned2019-05-13T09:02:32Z
dc.date.available2019-05-13T09:02:32Z
dc.date.issued2018
dc.identifier.issn1099-6362
dc.identifier.urihttps://doi.org/10.1177/1099636216629375
dc.identifier.urihttps://hdl.handle.net/11491/1274
dc.description.abstractHoneycomb sandwich structures are increasingly used in the automotive, aerospace and shipbuilding industries where fuel savings, increase in load carrying capacity, vehicle safety and decrease in gas emissions are very important aspects. The aim of this study was to develop the theoretical methods, initially proposed by the authors and by other researchers for the prediction of low-velocity impact responses of sandwich structures. The developed methods were applied to sandwich structures with aluminium honeycomb cores and glass-epoxy facings for the assessment of impact parameters and for the prediction of limit loads. The values of model parameters were compared with data reported in literature and the predictions of the limit loads were validated by means of the experimental data. Good achievement was obtained between the results of the theoretical models and the experimental data. The failure mode and the internal damage of the sandwich panels have been investigated using 3D computed tomography, which allowed the evaluation of parameters of energy balance model, and infrared thermography, which allowed the detection of the temperature evolution of the specimens during the tests. The experimental and theoretical results demonstrated that the use of glass-epoxy reinforcement on aluminium honeycomb sandwiches enhances the energy absorption and load carrying capacities. © 2016, © The Author(s) 2016.en_US
dc.language.isoeng
dc.publisherSAGE Publications Ltden_US
dc.relation.isversionof10.1177/1099636216629375en_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectaluminium honeycomb sandwich; computed tomography; infrared thermography; light-weight structures; Low-velocity impact; ship structuresen_US
dc.titleTheoretical and experimental analysis for the impact response of glass fibre reinforced aluminium honeycomb sandwichesen_US
dc.typearticleen_US
dc.relation.journalJournal of Sandwich Structures and Materialsen_US
dc.contributor.departmentHitit Universityen_US
dc.identifier.volume20en_US
dc.identifier.issue1en_US
dc.identifier.startpage42en_US
dc.identifier.endpage69en_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US


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