TY - JOUR
T1 - Studying the Tensile Behaviour of GLARE Laminates: A Finite Element Modelling Approach
AU - Soltani, Payam
AU - Keikhosravy, Mehdi
AU - Oskouei, Reza
AU - Soutis, Constantinos
PY - 2011/8
Y1 - 2011/8
N2 - Numerical simulations based on finite element modelling are increasingly being developed to accurately evaluate the tensile properties of GLARE (GLAss fibre REinforced aluminium laminates). In this study, nonlinear tensile behaviour of GLARE Fibre Metal Laminates (FML) under in-plane loading conditions has been investigated. An appropriate finite element modelling approach has been developed to predict the stress-strain response and deformation behaviour of GLARE laminates using the ANSYS finite element package. The finite element model supports orthotropic material properties for glass/epoxy layer(s) and isotropic properties with the elastic-plastic behaviour for the aluminium layers. The adhesion between adjacent layers has been also properly simulated using cohesive zone modelling. An acceptable agreement was observed between the model predictions and experimental results available in the literature. The proposed model can be used to analyse GLARE laminates in structural applications such as mechanically fastened joints under different mechanical loading conditions.
AB - Numerical simulations based on finite element modelling are increasingly being developed to accurately evaluate the tensile properties of GLARE (GLAss fibre REinforced aluminium laminates). In this study, nonlinear tensile behaviour of GLARE Fibre Metal Laminates (FML) under in-plane loading conditions has been investigated. An appropriate finite element modelling approach has been developed to predict the stress-strain response and deformation behaviour of GLARE laminates using the ANSYS finite element package. The finite element model supports orthotropic material properties for glass/epoxy layer(s) and isotropic properties with the elastic-plastic behaviour for the aluminium layers. The adhesion between adjacent layers has been also properly simulated using cohesive zone modelling. An acceptable agreement was observed between the model predictions and experimental results available in the literature. The proposed model can be used to analyse GLARE laminates in structural applications such as mechanically fastened joints under different mechanical loading conditions.
KW - Fibre Metal Laminates
KW - Finite element modelling
KW - GLARE
KW - Tensile behaviour
UR - http://www.scopus.com/inward/record.url?scp=80052437435&partnerID=8YFLogxK
U2 - 10.1007/s10443-010-9155-x
DO - 10.1007/s10443-010-9155-x
M3 - Article
SN - 0929-189X
VL - 18
SP - 271
EP - 282
JO - Applied Composite Materials
JF - Applied Composite Materials
IS - 4
ER -