2004
DOI: 10.1016/j.tws.2004.05.008
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Delamination buckling and postbuckling in composite cylindrical shells under external pressure

Abstract: Composite cylindrical shells and panels are widely used in aerospace structures. These are often subjected to defects and damage from both in-service and manufacturing events.Delamination is the most important of these defects. This paper deals with the computational modelling of delamination buckling and postbuckling of laminated composite cylindrical shells subjected to external pressure. The use of three-dimensional finite elements for predicting the delamination buckling and postbuckling of these structure… Show more

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Cited by 36 publications
(25 citation statements)
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“…Four different materials [16,17] are used to investigate the effect of engineering constants on the optimum shape design of the components. Every component is being treated as a lamina that has four engineering constants E 1 , E 2 , G 12 and  12 with a lamina orientation angle of zero.…”
Section: Numerical Resultsmentioning
confidence: 99%
“…Four different materials [16,17] are used to investigate the effect of engineering constants on the optimum shape design of the components. Every component is being treated as a lamina that has four engineering constants E 1 , E 2 , G 12 and  12 with a lamina orientation angle of zero.…”
Section: Numerical Resultsmentioning
confidence: 99%
“…Although cylinder tubes can fail in multiple ways under combined axial-pressure loadings (Marinucci and de Andrade, 2006;Tafreshi, 2004;Wiggenraad et al, 1996), delamination-type failure was commonly encountered in thick composite cylinders Rasheed and Tassoulas, 2001;Zhao et al, 2000). Potential delamination of the cylinder can be annular delamination (Kachanov, 1988), strip-type delamination and buckling of the delamination regions.…”
Section: Mechanical Behavior Modeling Of Composites Under Combined Lomentioning
confidence: 99%
“…Although cylinder tubes may fail in multiple ways under combined axialpressure loadings (Marinucci and de Andrade, 2006;Tafreshi, 2004;Wiggenraad et al, 1996), delamination-type failure was commonly encountered in thick composite cylinders (Bai et al, 1997;Rasheed and Tassoulas, 2001;Zhao et al, 2000). Potential delamination of the cylinder such as annular delamination (Kachanov, 1988), strip-type delamination (Timoshenko and Gere, 1961) and buckling of the delamination regions were numerically investigated by Theotokoglou (Theotokoglou, 2006).…”
Section: Numerical Analysismentioning
confidence: 99%