2017
DOI: 10.1007/s10443-017-9593-9
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A Multi Material Shell Model for the Mechanical Analysis of Triaxial Braided Composites

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Cited by 11 publications
(9 citation statements)
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“…In the case of ply architectures with higher complexity than unidirectional fibres, such as in textile composites, a subsequent homogenization step needs to be performed based on the previously computed behaviour of the unidirectional yarns, the response of the bulk resin matrix and on the topology of the Representative Unit Cell (RUC) of the fabric (e.g. [14][15][16][17]). From the orthotropic ply behaviour and lamina orientations within a ply stacking, computational mesomechanics can be used to predict the behaviour of the laminate (e.g.…”
Section: Introductionmentioning
confidence: 99%
“…In the case of ply architectures with higher complexity than unidirectional fibres, such as in textile composites, a subsequent homogenization step needs to be performed based on the previously computed behaviour of the unidirectional yarns, the response of the bulk resin matrix and on the topology of the Representative Unit Cell (RUC) of the fabric (e.g. [14][15][16][17]). From the orthotropic ply behaviour and lamina orientations within a ply stacking, computational mesomechanics can be used to predict the behaviour of the laminate (e.g.…”
Section: Introductionmentioning
confidence: 99%
“…A practical way for the analysis of a composite structure is to take an approach of a multi-scale framework (MSF) [ 68 , 69 , 70 , 71 , 72 , 73 , 74 ]. As shown in Figure 1 in the MSF the models at different scales are built independently but are combined organically so that loads and material data can be transferred between the models.…”
Section: Introductionmentioning
confidence: 99%
“…Characterisation and testing of braided composites loading cases are shown in Figure 3.21. In both cases, cracks were also generated at the yarn/matrix interface or grew from the inner region of the tows producing yarn to matrix interface debonding as identified in García-Carpintero et al (2017b) for tensile strength specimens. These tow/interface cracks grew stably in the fibre direction mainly driven by the resolved tensile and shear forces acting in this direction due to the applied normal stresses.…”
Section: Failure Mechanismsmentioning
confidence: 97%
“…However, these models require a considerable number of input properties, can be very complex to implement and their computational cost is high, Stig and Hallström (2012a). Computational efficiency is the biggest advantage of the CLT-models, which enable the implementation of material constitutive equations and can be used to solve structural problems using FE methods, García-Carpintero et al (2017b). The following section gives and overview of models for textile composite constitutive behaviour prediction, with a focus on models for braided composites.…”
Section: Modelling and Simulation Of Textile Compositesmentioning
confidence: 99%
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