2016
DOI: 10.1016/j.compstruct.2015.12.035
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Failure envelopes for laminated composites by the parametric HFGMC micromechanical framework

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Cited by 16 publications
(7 citation statements)
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“…subcell Ω pγq σ σ σ pγq " C pγq ε ε ε pγq subcell Ω pαq σ σ σ pαq " C pαq ε ε ε pαq zero-thickness interface S pkq s t pkq " p1´D pkq qΩ Ω Ω HOOKE's generalized model for each subcell Ω pβq of the discretized repeating unit cell (RUC) to represent volumetric damage, see [1] and Fig. 1 left.…”
Section: Micromechanical Modelsmentioning
confidence: 99%
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“…subcell Ω pγq σ σ σ pγq " C pγq ε ε ε pγq subcell Ω pαq σ σ σ pαq " C pαq ε ε ε pαq zero-thickness interface S pkq s t pkq " p1´D pkq qΩ Ω Ω HOOKE's generalized model for each subcell Ω pβq of the discretized repeating unit cell (RUC) to represent volumetric damage, see [1] and Fig. 1 left.…”
Section: Micromechanical Modelsmentioning
confidence: 99%
“…The subcells do not damage in this approach but follow HOOKE's model. The continuity and periodicity of tractions and displacements along the subcell boundaries of the RUC, as well as the static equilibrium in each subcell need to be satisfied in the high-fidelity generalized method of cells (HFGMC) in an integral average, see [1,3]. A system of nonlinear equations is obtained by evaluating these conditions and taking evolving continuum damage into account.…”
Section: Micromechanical Modelsmentioning
confidence: 99%
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“…For overcoming the microscopic local stress concentration between inclusions and matrix due to the regular discrete elements, an isoparametric element is employed by Haj-Ali and Aboudi (2013) and Ye et al (2015a). Levi-Sasson et al (2016) constructed the parametric HFGMC to determine the failure envelopes of composite materials. The micromechanical model was proved to be effectiveness in predicting the multi-axis stress failures.…”
Section: Introductionmentioning
confidence: 99%