2018
DOI: 10.1007/s10443-018-9732-y
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Multi-Scale Progressive Damage Model for Analyzing the Failure Mechanisms of 2D Triaxially Braided Composite under Uniaxial Compression Loads

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Cited by 19 publications
(7 citation statements)
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“…This type of damage mode is due to the fact that the inconsistent deformation occurs between the pure matrix and tows, leading to the shearing force. The predicted results agree well with the meso-scale simulation results from Zhang et al (2018) and Ren et al (2018). In addition, it is found from Figure 16 that the interface debonding is distributed dispersedly at the whole model.…”
Section: Multi-scale Model Validationsupporting
confidence: 82%
See 1 more Smart Citation
“…This type of damage mode is due to the fact that the inconsistent deformation occurs between the pure matrix and tows, leading to the shearing force. The predicted results agree well with the meso-scale simulation results from Zhang et al (2018) and Ren et al (2018). In addition, it is found from Figure 16 that the interface debonding is distributed dispersedly at the whole model.…”
Section: Multi-scale Model Validationsupporting
confidence: 82%
“…Recently, the meso-scale finite element method (FEM) being capable of capturing detailed damage information of tow has been widely used to analyze the mechanical behaviors of 2DTBC. For example, Nie and Binienda (2015), Li et al (2010), Zhang et al (2018), Ren et al (2018) and Jiang et al (2018aJiang et al ( , 2018b) simulated the internal damage behaviors of 2DTBC under different loading based on the meso-scale FEM. They established the Representative Volume Element (RVE) model of 2DTBC and developed the effective meso-mechanical damage models.…”
Section: Introductionmentioning
confidence: 99%
“…Braided composites have been widely used in aerospace due to their excellent properties, such as high stiffness, high strength to weight ratio, and good fatigue strength [ 1 , 2 , 3 ]. They can reduce the use of high alloy on the aircraft, save on structural costs, and have a great advantage in weight reduction and efficiency.…”
Section: Introductionmentioning
confidence: 99%
“…Ye et al 20 modified the concentric cylindrical model and rule of mixtures relations to derive a numerical model for the estimation of mechanical properties for the TBC made of anisotropic carbon fibres. Zhang et al 21 developed a multi-scale damage model of study of the progressive failure mechanism of the TBC subjected to uniaxial compressive loads. In this study, pure matrix cracking and interface debonding were the observed failure modes under transverse compression.…”
Section: Introductionmentioning
confidence: 99%