Damage evolution in open-hole laminated composite plates subjected to in-plane loads

Home | About RECERCAT | Contact

Català | Castellano

All of RECERCAT

By Communities &
Collections By Defense Date By Authors By Titles By Subject

This Collection

By Defense Date By Authors By Titles By Subject

Statistics

View Statistics All RECERCAT

My RECERCAT

Other repositories directory

RECERCAT Home > Universitat Politècnica de Catalunya > Documents de recerca > View document

To access the full text documents, please follow this link: http://hdl.handle.net/2117/86266

dc.contributor	Universitat Politècnica de Catalunya. Departament de Física
dc.contributor	Universitat Politècnica de Catalunya. RMEE - Grup de Resistència de Materials i Estructures en l'Enginyeria
dc.contributor.author	Moure, M. M.
dc.contributor.author	Otero Gruer, Fermín Enrique
dc.contributor.author	Garcia Castillo, S. K.
dc.contributor.author	Sanchez Saez, S.
dc.contributor.author	Barbero, E
dc.contributor.author	Barbero, Ever
dc.date	2015-12-01
dc.identifier.citation	Moure, M.M., Otero, F., Garcia, S., Sanchez, S., Barbero, E., Barbero, E. Damage evolution in open-hole laminated composite plates subjected to in-plane loads. "Composite structures", 01 Desembre 2015, vol. 133, p. 1048-1057.
dc.identifier.citation	0263-8223
dc.identifier.citation	10.1016/j.compstruct.2015.08.045
dc.identifier.uri	http://hdl.handle.net/2117/86266
dc.language.iso	eng
dc.relation	http://www.sciencedirect.com/science/article/pii/S0263822315007229
dc.rights	info:eu-repo/semantics/openAccess
dc.rights	http://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.subject	Àrees temàtiques de la UPC::Enginyeria dels materials::Assaig de materials
dc.subject	Composite materials
dc.subject	Strength of materials
dc.subject	Discrete damage mechanics
dc.subject	open-hole composite laminates
dc.subject	ultimate strength
dc.subject	stress redistribution
dc.subject	notched composites
dc.subject	strength
dc.subject	model
dc.subject	failure
dc.subject	tensile
dc.subject	mechanisms
dc.subject	prediction
dc.subject	cracking
dc.subject	Materials compostos
dc.subject	Resistència de materials
dc.title	Damage evolution in open-hole laminated composite plates subjected to in-plane loads
dc.type	info:eu-repo/semantics/submittedVersion
dc.type	info:eu-repo/semantics/article
dc.description.abstract	Damage evolution of notched composite laminates is analysed in this work using a discrete damage model, which estimates matrix damage evolution and fibre failure. The fibre damage is regularised with a Weibull distribution, and a Regula Falsi method has been used to improve numerical convergence. The model is compared and validated with several experimental results taken from the scientific literature, which consider different materials, laminate stacking sequences and specimen geometries. A good correlation has been found for the failure strength and the stress strain curve of notched and un-notched laminates subjected to in plane loads. The influence of the Weibull modulus on the matrix and fibre damage evolution, and the failure strength, is analysed. (C) 2015 Elsevier Ltd. All rights reserved.
dc.description.abstract	Peer Reviewed

Show simple item record

All of RECERCAT

This Collection

Statistics

My RECERCAT

Related documents

Other documents of the same author