2014
DOI: 10.1016/j.compositesa.2013.10.002
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Numerical simulation of strain-rate dependent transition of transverse tensile failure mode in fiber-reinforced composites

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Cited by 35 publications
(21 citation statements)
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“…11, the plastic strain around the crack site increases with decreasing angle. Koyanagi et al (2014) experimentally demonstrated that the morphology of the matrix crack depends on the strain rates, and we also simulated the dependency using the unit cell. Fig.…”
Section: Initial Cracks In Composite Laminatesmentioning
confidence: 97%
See 1 more Smart Citation
“…11, the plastic strain around the crack site increases with decreasing angle. Koyanagi et al (2014) experimentally demonstrated that the morphology of the matrix crack depends on the strain rates, and we also simulated the dependency using the unit cell. Fig.…”
Section: Initial Cracks In Composite Laminatesmentioning
confidence: 97%
“…Asp et al (1996aAsp et al ( , 1996b presented the failure process based on the dilatation energy criterion, and Okabe et al (2011) simulated the cracking strain using the periodic unit cell and modified Gurson Law. Moreover, Sato et al (2014) successfully used a combination of the dilatation energy criterion and the modified Gurson Law to predict the cracking strain of an off-axis ply. As shown in Fig.…”
Section: Initial Cracks In Composite Laminatesmentioning
confidence: 99%
“…Tabiei et al [19][20][21][22] developed a finite element method to consider the nonlinearity and dynamic sensitivity in calculating mechanical properties of fibrous composites by using the Goldberg model for polymers [25]. Koyanagi et al [26] studied the strain rate dependent transverse tensile of UD composites numerically. Although the fiber, matrix and interface have been modeled individually, but the aim of their study was investigating the failure modes of UD composites under strain rate dependent transverse tensile loadings.…”
Section: Introductionmentioning
confidence: 99%
“…In particular, intralaminar failure, including matrix failure and interfacial debonding, or interlaminar failure between neighboring laminae is more important than the final failure that comes with fiber breakage in CFRP structures under operation. Initiation and progress of transverse cracks, which are the main initial failure modes of CFRP laminates, have been analyzed by considering matrix failure and interfacial debonding (Okabe et al, 2011(Okabe et al, , 2015Koyanagi et al, 2014). It has been reported that such transverse crack tends to occur in a relatively low stress level and is strongly affected by interfacial properties between carbon fibers and a matrix resin.…”
Section: Introductionmentioning
confidence: 99%