2018
DOI: 10.1016/j.compstruct.2018.04.005
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Influence of stiffener configuration on post-buckled response of composite panels with impact damages

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Cited by 15 publications
(7 citation statements)
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“…Even though stiffened panels CAI numerical studies have been undertaken by many researchers [3], [9], [14], [17], [18], [22]- [26], the inefficient convergence behaviour of the CZM method is emphasised in many studies [9], [14], [18], [22], [24], [26]. In this paper, parametric analyses were conducted to investigate the optimum CAI modelling strategy and the effect of the critical parameters involved on the accuracy and computational efficiency.…”
Section: Resultsmentioning
confidence: 99%
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“…Even though stiffened panels CAI numerical studies have been undertaken by many researchers [3], [9], [14], [17], [18], [22]- [26], the inefficient convergence behaviour of the CZM method is emphasised in many studies [9], [14], [18], [22], [24], [26]. In this paper, parametric analyses were conducted to investigate the optimum CAI modelling strategy and the effect of the critical parameters involved on the accuracy and computational efficiency.…”
Section: Resultsmentioning
confidence: 99%
“…The required number of cohesive zones that lead to an accurate simulation was questioned. In similar CAI studies, the most common method is to use cohesive elements in the interface between the skin and the stiffener as shown in figure 10 [3], [9], [17]. On the other hand, in impact studies, cohesive elements may be applied even between all the adjacent plies [34], nevertheless, the scope of these is different to the CAI simulations.…”
Section: • Required Number Of Cohesive Zones Within the Numerical Modelmentioning
confidence: 99%
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