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dc.contributor.authorRastellini, Fernando G.
dc.contributor.authorSalomón, Ramón Omar
dc.contributor.authorOller Martínez, Sergio Horacio
dc.contributor.authorOñate Ibáñez de Navarra, Eugenio
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament d'Enginyeria Civil i Ambiental
dc.date.accessioned2017-10-31T12:39:40Z
dc.date.available2017-10-31T12:39:40Z
dc.date.issued2006
dc.identifier.citationRastellini, F.G., Salomon Rotlisbeger, Ramon Omar, Oller, S., Oñate, E. Non-linear mechanical damage modelling for long fibre-reinforced laminates. A: Conference on Damage in Composite Materials. "CDCM 2006: Conference on Damage in Composite Materials 2006, 18th-19th of September 2006 in Stuttgart, Germany: online-proceedings". Stuttgart: 2006, p. 1-11.
dc.identifier.urihttp://hdl.handle.net/2117/109513
dc.description.abstractA computational methodology is presented for modelling the material non-linear mechanical behaviour of composite structures made of FRP (Fibre-Reinforced Plastic) laminates. The model is based on the appropriate combination of the constitutive models of component materials, considered to behave as isolated continua, together with additional ‘closure equations’ that characterize the micromechanics of the composite from a morphological point of view. To this end, any appropriate constitutive model may be selected for each phase. Each component is modelled separately and the global response is obtained by assembling all contributions taking into account the interactions between components in a general phenomenological way. To model the behaviour of a single unidirectional (UD) composite lamina, a Serial-Parallel continuum approach has been developed assuming that components behave as parallel materials in the fibres alignment direction and as serial materials in orthogonal directions. Taking into account the internal morphology of the composite material, it is devised a strategy for decoupling and coupling component phases. This methodology [1], named “compounding of behaviours”, allows to take into consideration local degradation phenomena (in the constituents materials), like plasticity, damage, fatigue [2], etc. in a coupled manner. It is based on the proper management of homogenous constitutive models, already available for each component. In this way, it is used all developments achieved in constitutive modelling of plain materials, what makes possible the transference of this technology to composites. A lamination theory complemented with the proposed UD model is employed to describe the mechanical behaviour of multidirectional laminates. A specific solution strategy for the general non linear case is proposed. It provides quick local and global convergences, what makes the model suitable for large scale structures. The model brings answers on the non-linear behaviour of composites, where classical micro-mechanics formulas are restricted to their linear elastic part. The methodology is validated through several numerical analyses and contrasted against experimental data and benchmark tests.
dc.format.extent11 p.
dc.language.isoeng
dc.subjectÀrees temàtiques de la UPC::Enginyeria civil::Materials i estructures
dc.subject.lcshFiber-reinforced plastics--Testing
dc.subject.otherFRP composite laminates
dc.subject.otherNon-linear continuum damage modelling
dc.subject.otherFailure envelopes
dc.subject.otherFEA
dc.titleNon-linear mechanical damage modelling for long fibre-reinforced laminates
dc.typeConference report
dc.subject.lemacPlàstics reforçats amb fibra -- Proves
dc.contributor.groupUniversitat Politècnica de Catalunya. GMNE - Grup de Mètodes Numèrics en Enginyeria
dc.contributor.groupUniversitat Politècnica de Catalunya. (MC)2 - Grup de Mecànica Computacional en Medis Continus
dc.relation.publisherversionhttp://www.ndt.net/article/cdcm2006/papers/rastellini.pdf
dc.rights.accessOpen Access
drac.iddocument2344683
dc.description.versionPostprint (published version)
upcommons.citation.authorRastellini, F.G.; Salomon Rotlisbeger, Ramon Omar; Oller, S.; Oñate, E.
upcommons.citation.contributorConference on Damage in Composite Materials
upcommons.citation.pubplaceStuttgart
upcommons.citation.publishedtrue
upcommons.citation.publicationNameCDCM 2006: Conference on Damage in Composite Materials 2006, 18th-19th of September 2006 in Stuttgart, Germany: online-proceedings
upcommons.citation.startingPage1
upcommons.citation.endingPage11


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