Predictive model for the spherical indentation of composite laminates with finite thickness
dc.contributor.author
dc.date.accessioned
2016-11-17T11:12:12Z
dc.date.available
2016-11-17T11:12:12Z
dc.date.issued
2016-10-01
dc.identifier.issn
0263-8223
dc.identifier.uri
dc.description.abstract
The elastic response of composite laminates in contact with a stiff indenter is of immense importance in many applications. With the aim to further extend the knowledge on this subject, the contact problem of a stiff spherical indenter with a composite plate was simulated with a 2D axisymmetric model implemented on a commercial software. A parametric study was carried out numerically to study the effect of the different parameters on the force–indentation response. The results show that the indentation response of an orthotropic laminate is material independent and that it strongly depends on the laminate thickness. The lamina thickness has no significant effect on the force–indentation relation. Also, the effect of hole radius can be neglected for the hollow support experiment. Two simple equations were derived by normalizing and fitting FE results to predict the response of an orthotropic laminate of finite thickness in contact with stiff spherical indenter supported on two different boundary conditions (fully and hollow supported). The predictions of the derived equations were compared with experimental results and the available analytical models in the literature. The presented equations show an excellent correlation with the experimental investigations
dc.description.sponsorship
This work has been partially funded by the Spanish Government (Ministerio de Economia y Competitividad) and the European Union under contracts DPI2012-34465 and MAT2013-46749-R
dc.format.mimetype
application/pdf
dc.language.iso
eng
dc.publisher
Elsevier
dc.relation
info:eu-repo/grantAgreement/MINECO//DPI2012-34465/ES/EVALUACION DE COMPOSITES LAMINADOS DE CAPAS FINAS PARA APLICACIONES AERONAUTICAS Y AEROESPACIALES/
info:eu-repo/grantAgreement/MINECO//MAT2013-46749-R/ES/DIAGRAMAS DE FACTORES DE CONCENTRACION DE TENSIONES PARA MATERIALES CASI-FRAGILES/
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Reproducció digital del document publicat a: http://dx.doi.org/10.1016/j.compstruct.2016.06.056
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© Composite Structures, 2016, vol. 153, p. 468-477
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Articles publicats (D-EMCI)
dc.rights
Tots els drets reservats
dc.subject
dc.title
Predictive model for the spherical indentation of composite laminates with finite thickness
dc.type
info:eu-repo/semantics/article
dc.rights.accessRights
info:eu-repo/semantics/embargoedAccess
dc.embargo.terms
Cap
dc.date.embargoEndDate
info:eu-repo/date/embargoEnd/2026-01-01
dc.type.version
info:eu-repo/semantics/publishedVersion
dc.identifier.doi
dc.identifier.idgrec
025576
dc.contributor.funder
dc.relation.ProjectAcronym
dc.identifier.eissn
1879-1085