Numerical Simulation of Mixed-Mode Progressive Delamination in Composite Materials

By Pedro P. Camanho, C. Dávila, M. D. De Moura. 2003

1,711 citations recorded by the source corpus.

Subfields: Building and Construction, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/a6b09f568c921823eb83e7bbaf2526c51841681c

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In Building and Construction

In Mechanics of Materials

Citations in the corpus

A crack tip tracking algorithm for cohesive interface element analysis of fatigue delamination propagation in composite materials (2012, background): “In standard cohesive element formulations the degradation of the interface is characterised by the loss of cohesive stiffness which is represented by a scalar damage variable (Chen et al., 1999; Alfano and Crisfield, 2001; Camanho et al., 2003).”
Numerical modelling of the damage modes in UD thin carbon/glass hybrid laminates (2014, methodology): “A bilinear cohesive law based on the formulation of [10] with no permanent deformation in the unloading path is used for the cohesive elements.”
A phantom node formulation with mixed mode cohesive law for splitting in laminates (2009, methodology): “Material parameters from Camanho et al. (2003) for carbon/PEEK fiber reinforced composite are used (see Table 1).”
A review of strategies for improving the degradation properties of laminated continuous-fiber/epoxy composites with carbon-based nanoreinforcements (2012, background): “These are two distinct parameters in any structural delamination model based on cohesive or interface elements [19,123,33,124].”
Formulation and implementation of decohesion elements in an explicit finite element code (2006, methodology): “previous section, for consistency with the work on which it was based [1,9, 6 ].”
A fatigue degradation law for cohesive interface elements – Development and application to composite materials (2010, background): “Interface elements are becoming widely used to predict such delamination failures [2,3,4,5,6,7].”
A damage model for the simulation of delamination in advanced composites under variable-mode loading (2006, methodology): “The law proposed here is a bilinear relation between the tractions and the displacement jumps [21],[24],[45].”