2012
DOI: 10.1016/j.compstruct.2011.12.030
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Numerical investigation into multi-delamination failure of composite T-piece specimens under mixed mode loading using a modified cohesive model

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Cited by 20 publications
(13 citation statements)
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“…Where, is the damaged elasticity matrix formulated mathematically based on scalar damage approach defined in Equation 7, which was proposed by previous researchers including [27][28][29][30][31][32][33] (1 )…”
Section: An Ageing Concrete Materials Modelmentioning
confidence: 99%
“…Where, is the damaged elasticity matrix formulated mathematically based on scalar damage approach defined in Equation 7, which was proposed by previous researchers including [27][28][29][30][31][32][33] (1 )…”
Section: An Ageing Concrete Materials Modelmentioning
confidence: 99%
“…In the general mixed damage mode case, two quadratic formulas given in previous work [18][19] Firstly, assume the amount of total damage scale in mixed facture mode case equals the value of damage scale in the pure single mode I case. This can be expressed by equ.…”
Section: (17)mentioning
confidence: 99%
“…The literature survey of T-joints shows that filler region and flange tips are the critical locations for delamination/debond initiation. Two of the major initiation mechanisms observed in the literature are the debond of the filler/stringer interface [10,19,23] as shown in Figure 3 and the delamination of plies in the stringer laminate at the curved region [1,3,4,6] as shown in Figure 4. …”
Section: Critical Regions In T-joints For Delamination/debondmentioning
confidence: 99%