2022
DOI: 10.1016/j.ijmecsci.2022.107298
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A coupled plasticity-damage cohesive-frictional interface for low-cycle fatigue analysis

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Cited by 10 publications
(5 citation statements)
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“…First, including a suitable representation of intergranular damage evolution [87,88,27,29,89], the framework could be extended for the investigation of thermo-mechanic micro-cracking in brittle and quasi-brittle materials, both in a steady-state and transient setting [90,91]. In this respect, it might be observed that the dependence of the material coefficients on the temperature, i.e.…”
Section: Discussion and Further Developmentsmentioning
confidence: 99%
“…First, including a suitable representation of intergranular damage evolution [87,88,27,29,89], the framework could be extended for the investigation of thermo-mechanic micro-cracking in brittle and quasi-brittle materials, both in a steady-state and transient setting [90,91]. In this respect, it might be observed that the dependence of the material coefficients on the temperature, i.e.…”
Section: Discussion and Further Developmentsmentioning
confidence: 99%
“…From a more physical point of view, the model could be extended considering other damage mechanisms such as inter-laminar delamination or impact induced damage. Delamination could be modelled by using layer-wise displacement approximations along the thickness, hybrid variational statements [52], and cohesive inter-laminar traction-separation laws [53,54]. These tools would provide a direct representation of the displacement jumps between contiguous layers and their relation with the inter-laminar damage up to complete decohesion.…”
Section: Discussionmentioning
confidence: 99%
“…The extrinsic interface is modelled in the present article by the rigid‐damage CZM proposed by the Author in References 42,55,56 in the rigorous thermodynamic framework of damage mechanics. The CZM is hereafter developed in a complementary form starting from the following Gibbs free energy function, defined for a unit of interface surface, G(bold-italics,ω)=12ω1prefix−ωbold-italicsTboldAelbold-italics,$$ G\left(\boldsymbol{s},\omega \right)=\frac{1}{2}\frac{\omega }{1-\omega }{\boldsymbol{s}}^T{\mathbf{A}}^{el}\boldsymbol{s}, $$ where 0ω1$$ 0\le \omega \le 1 $$ is the scalar damage variable.…”
Section: Hee With Embedded Extrinsic Interfacementioning
confidence: 99%