A thermomechanical constitutive theory for elastic composites with distributed damage—II. Application to matrix cracking in laminated composites
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Cited by (146)
Modelling damage evolution in multidirectional laminates: Micro to macro
2020, Multi-Scale Continuum Mechanics Modelling of Fibre-Reinforced Polymer CompositesState of the art in fatigue modelling of composite wind turbine blades
2018, International Journal of FatigueCitation Excerpt :As for Diao et al. he established a statistical equation of residual strength evolution controlling the global uniaxial [116] and multiaxial [117] stiffness reduction of composite laminae. Another model has been developed by Allen et al. [50], which sources a mixture of micro-mechanical and phenomenological solutions to derive constitutive equations at the ply level. The constitutive equations are constructed using thermodynamics-related constraints, and depend on internal state variables.
Durability of composite materials during hydrothermal and environmental aging
2018, Durability and Life Prediction in Biocomposites, Fibre-Reinforced Composites and Hybrid CompositesFinite strip modeling of cementitious laminates reinforced with sisal fibers
2015, Cement and Concrete CompositesCitation Excerpt :In this case, only the extensional deformations are considered [25,26]. Based on the continuous damage theory, many works have also been developed to analyze cracks in the matrix, fiber-matrix de-bonding and inter-lamina cracks [27–29]. Thus, from the association between the CTL and DM, it is possible to define a failure criterion for each lamina of the composite, associated with tensile strength, compressive strength or interface strength [16,17].
Intra and damage analysis of laminated composites using coupled continuum damage mechanics with cohesive interface layer
2015, Composite StructuresCitation Excerpt :It is worth noting that CDM has been firstly used for damage analysis of transversely isotropic composites by Talreja [14]. Also there has been an enormous effort to develop CDM in composite materials by Voyiadjis [29], Talreja [30,31], Ladevèze [32,33], and Barbero [34–36], Talreja [14,37], Lene [38], and Allen [39,40], and [41]. Talreja [14] proposed a second-order tensorial damage parameter, representing the damage effects in each density of matrix cracks.
Fatigue damage modelling of composite materials with the phenomenological residual stiffness approach
2010, Fatigue Life Prediction of Composites and Composite Structures