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2008
DOI: 10.1016/j.compstruc.2008.02.001
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Optimum topological design of simply supported composite stiffened panels via genetic algorithms

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Cited by 29 publications
(13 citation statements)
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“…Leheta and Mansour [13] developed a reliability-based methodology for structural optimization of stiffened panels which are typical of those found in the deck or bottom of longitudinally stiffened ships. Other optimization strategies such as the genetic algorithm and response surface method were also employed in the optimal design of stiffened plates and composite stiffened panels by Nagendra et al [14], Iuspa and Ruocco [15], Badran et al [16] and Rikardsa et al [17,18]. Many of the previous studies were based on eigenvalue buckling analyses and little research has been concerned with limit-point buckling analyses.…”
Section: Numbers Of X-stiffeners and Y-stiffeners Amentioning
confidence: 97%
“…Leheta and Mansour [13] developed a reliability-based methodology for structural optimization of stiffened panels which are typical of those found in the deck or bottom of longitudinally stiffened ships. Other optimization strategies such as the genetic algorithm and response surface method were also employed in the optimal design of stiffened plates and composite stiffened panels by Nagendra et al [14], Iuspa and Ruocco [15], Badran et al [16] and Rikardsa et al [17,18]. Many of the previous studies were based on eigenvalue buckling analyses and little research has been concerned with limit-point buckling analyses.…”
Section: Numbers Of X-stiffeners and Y-stiffeners Amentioning
confidence: 97%
“…A wide range of numerical methods are available, some which will require a smaller number of elements to accurately represent buckling behaviour, i.e. the finite strip method [22][23][24]. As a result, a FE approach is not the most efficient method however the additional computational burden is offset by the absence of any limitations on the geometry and boundary conditions that may be modelled.…”
Section: Finite Element Methodsmentioning
confidence: 99%
“…Recently, Nguyen et al [27] proposed a vibration and lateral buckling GA optimization of thin-walled laminated composite beams with channel sections, by considering flanges width, web height and fibre orientation as the design variables. Iuspa and Ruocco [28] and, more recently, Ehsani and Rezaeepazhand [29] proposed the stacking sequence optimization of laminated plates for maximum buckling load using GA.…”
Section: Introductionmentioning
confidence: 99%