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dc.rights.licenseopenen_US
dc.contributor.authorRAMAKRISHNAN, Karthik Ram
hal.structure.identifierInstitut de Mécanique et d'Ingénierie [I2M]
dc.contributor.authorGUÉRARD, Sandra
dc.contributor.authorZHANG, Zhifang
dc.contributor.authorSHANKAR, Krishna
hal.structure.identifierInstitut de Mécanique et d'Ingénierie [I2M]
dc.contributor.authorVIOT, Philippe
dc.date.accessioned2021-12-14T15:25:20Z
dc.date.available2021-12-14T15:25:20Z
dc.date.issued2019-06-11
dc.identifier.issn1099-6362en_US
dc.identifier.urioai:crossref.org:10.1177/1099636219856537
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/124165
dc.description.abstractEnSandwich composites with fibre-reinforced plastic facesheets and foam core have emerged as a major class of lightweight structural materials but low-velocity impact damage severely reduces the structural integrity of the component. Different methods have been proposed to improve the impact damage resistance of sandwich composites including the addition of nanoparticles to the matrix. The objective of this paper is to evaluate the effect of adding nanostrength, a block copolymer that self-assembles in the nanoscale, to the epoxy matrix on the low-velocity impact behaviour of sandwich panels with Kevlar facesheets and Rohacell foam core. Most previous studies on low-velocity impact damage used experimental testing but a combination of improved constitutive modelling of constituents and decreased computational costs make it possible to utilise continuum modelling to numerically simulate impact response of sandwich composites for a much wider range of conditions. A numerical model was developed in explicit FE software LS-Dyna and a constitutive law based on continuum damage mechanics was used for the simulation of the composite facesheets with and without the nano-reinforcements. A crushable foam model was used for the Rohacell foam core. The LS-Dyna model was validated by comparing the force, displacement measurements and damage assessment from the simulation with experimental impact tests conducted using a drop tower. The FE model shows good comparison with the experiment and a macroscopic phenomenological model is capable of capturing the impact damage behaviour of the sandwich plates with nano-reinforcements.
dc.language.isoENen_US
dc.sourcecrossref
dc.subject.enSandwich
dc.subject.enlow-velocity impact
dc.subject.enblock copolymer
dc.subject.enfinite element analysis
dc.subject.encontinuum damage mechanics
dc.subject.ennanoparticles
dc.title.enNumerical modelling of foam-core sandwich panels with nano-reinforced composite facesheets
dc.typeArticle de revueen_US
dc.identifier.doi10.1177/1099636219856537en_US
dc.subject.halSciences de l'ingénieur [physics]/Matériauxen_US
bordeaux.journalJournal of Sandwich Structures and Materialsen_US
bordeaux.page109963621985653en_US
bordeaux.volume23en_US
bordeaux.hal.laboratoriesInstitut de Mécanique et d’Ingénierie de Bordeaux (I2M) - UMR 5295en_US
bordeaux.issue4en_US
bordeaux.institutionUniversité de Bordeauxen_US
bordeaux.institutionBordeaux INPen_US
bordeaux.institutionCNRSen_US
bordeaux.institutionINRAEen_US
bordeaux.institutionArts et Métiersen_US
bordeaux.peerReviewedouien_US
bordeaux.inpressnonen_US
bordeaux.import.sourcedissemin
hal.identifierhal-03480404
hal.version1
hal.date.transferred2021-12-14T15:25:24Z
hal.exporttrue
workflow.import.sourcedissemin
dc.rights.ccPas de Licence CCen_US
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