A three-dimensional viscoelastic–viscoplastic and viscodamage constitutive model for unidirectional fibre-reinforced polymer laminates
dc.contributor.author
dc.date.accessioned
2024-07-02T08:09:50Z
dc.date.available
2024-07-02T08:09:50Z
dc.date.issued
2024-07-26
dc.identifier.issn
0266-3538
dc.identifier.uri
dc.description.abstract
A novel 3D viscoelastic–viscoplastic and viscodamage constitutive model is proposed to predict the viscous effects due to dynamic loading conditions of unidirectional carbon fibre-reinforced polymer laminates at the meso-scale level. The present model is developed under continuum damage mechanics and the thermodynamics of irreversible processes framework. The viscoelastic response is modelled using the generalised Maxwell model, while an overstress model is employed to address the viscoplastic strain. The onset of the viscodamage mechanisms is based on experimental expressions, and their propagation is defined as a function of the corresponding fracture toughness. The mechanical response of the present constitutive model under pure longitudinal shear loading conditions at different strain rates is presented. The higher the strain rate is, the stiffer the responses in the viscoelastic and viscoplastic regions are. Additionally, the onset of viscodamage increases with higher strain rates. Off-axis compressive experimental data at two different strain rates are employed to demonstrate the capabilities of the present model with good predictions being obtained
dc.description.sponsorship
The first author would like to acknowledge the support of the Catalan Government (Agència de Gestió d’Ajuts Universitaris i de Recerca) through Grant 2019FI_B_01117. The present research project has received funding from the Clean Sky 2 Joint Undertaking (JU) under grant agreements No. 886519 (BEDYN). The JU receives support from the European Union’s Horizon 2020 Research and Innovation programme and the Clean Sky 2 JU members other than the Union. The authors would also like to express special thanks to the Topic Managers of said European project for their support in the development of the work presented: Dassault Aviation. Grant PID2022-137979OB-I00 funded by MICIU/AEI/10.13039/501100011033 and by FEDER-European Union
Open Access funding provided thanks to the CRUE-CSIC agreement with Elsevier
dc.format.mimetype
application/pdf
dc.language.iso
eng
dc.publisher
Elsevier
dc.relation
PID2022-137979OB-I00
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Reproducció digital del document publicat a: https://doi.org/10.1016/j.compscitech.2024.110634
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Composites Science and Technology, 2024, vol. 254, art. núm. 110634
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Articles publicats (D-EMCI)
dc.rights
Attribution-NonCommercial-NoDerivatives 4.0 International
dc.rights.uri
dc.subject
dc.title
A three-dimensional viscoelastic–viscoplastic and viscodamage constitutive model for unidirectional fibre-reinforced polymer laminates
dc.type
info:eu-repo/semantics/article
dc.rights.accessRights
info:eu-repo/semantics/openAccess
dc.relation.projectID
info:eu-repo/grantAgreement/EC/H2020/886519/EU/Development of a methodology (test, measurement, analysis) to characterize the BEhaviour of composite structures under DYNamic loading/BEDYN
info:eu-repo/grantAgreement/AEI/Plan Estatal de Investigación Científica y Técnica y de Innovación 2021-2023/PID2022-137979OB-I00/ES/CARACTERIZACION MECANICA DE LA PROPAGACION DE GRIETAS BAJO CARGAS DINAMICAS EN COMPOSITES DE MATRIZ POLIMERICA AVANZADA Y RECUPERABLE PARA APLICACIONES DE TRANSPORTE/
dc.type.version
info:eu-repo/semantics/publishedVersion
dc.identifier.doi
dc.identifier.idgrec
039011
dc.contributor.funder
dc.type.peerreviewed
peer-reviewed
dc.relation.FundingProgramme
dc.relation.ProjectAcronym
dc.identifier.eissn
1879-1050