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Fatigue crack growth in thin notched woven glass composites under tensile loading. Part II: modelling

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Figure

Fig. 1. 1D modelling approach for a woven ply.
Fig. 3. Identification of the model coefficients in static tensile test for warp (a) and weft (b) directions.
Fig. 5. Predicted and experimental deformed shape for [45] 2 laminate in static tensile configuration.
Fig. 7. Fatigue stiffness degradation of links elements vs. maximum fatigue strain of fibres.
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