American Society for Composites 2020 2020
DOI: 10.12783/asc35/34953
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An Automated Meshing Framework for Progressive Damage Analyss of Fabrics Using CompDam

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Cited by 4 publications
(6 citation statements)
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“…A slightly lower value is obtained for the unit cell with identical topology using DFCA. Since the actual cross-section area in the loading direction is unavailable from the literature, the corrected cross-sectional area, A e , is calculated to determine the nominal stress σ x , according to equation (15). A and v f are the nominal area and overall fiber volume fraction from DFCA, whereas A e and v e f are those from the experimental data.…”
Section: Resultsmentioning
confidence: 99%
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“…A slightly lower value is obtained for the unit cell with identical topology using DFCA. Since the actual cross-section area in the loading direction is unavailable from the literature, the corrected cross-sectional area, A e , is calculated to determine the nominal stress σ x , according to equation (15). A and v f are the nominal area and overall fiber volume fraction from DFCA, whereas A e and v e f are those from the experimental data.…”
Section: Resultsmentioning
confidence: 99%
“…27 Bergan used a CDM model with cohesive zone elements to model damage inside yarns and on yarn-matrix interfaces, while matrix damage is accounted for by plasticity. 15 Saleh et al proposed a micro-mechanical model to simulate tensile response of woven composites using damage evolution laws governed by material parameters. 28 Bogdanovich et al used the 3D Mosaic concept to represent the woven composite structure as an assembly of an arbitrary number of distinct homogeneous anisotropic material blocks.…”
Section: Introductionmentioning
confidence: 99%
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“…Although TexGen has many advantages, there is still a lack of complete automation tools for modeling, simulation and post-processing of woven composite. In addition, fabric modeling and analysis programs such as WiseTex, 19 CompDam, 20 DFCA, 21 and NASMAT 22 have been developed for multi-scale analysis. However, computational cost can be exorbitant as many of the models contain upwards of hundreds of thousands, or even millions, of degrees of freedom to admit the necessary geometric complexity.…”
Section: Introductionmentioning
confidence: 99%
“…Some models have been developed to investigate the effects of damage at the various length scales present in 3D woven composites [ 1 , 2 , 3 , 4 , 5 , 6 , 7 , 8 ]. However, when looking at the broader 3D woven-composite modeling literature, the trend is to use highly-refined finite element models of the woven architecture at a single scale [ 9 , 10 , 11 , 12 , 13 , 14 , 15 , 16 , 17 , 18 , 19 , 20 , 21 , 22 , 23 , 24 ], and multiscale models are generally not employed due to prohibitive computational costs. As a result of the high computational demand for high-fidelity finite element models, particularly in the context of progressive failure analysis, it is currently challenging to perform sensitivity or optimization analyses for 3D woven composites based on this approach.…”
Section: Introductionmentioning
confidence: 99%