Int. J. Simul. Multidisci. Des. Optim.
Volume 2, Number 2, April 2008
Composite and Aircraft Materials
|Page(s)||101 - 106|
|Published online||22 May 2008|
Incorporating industrial constraints for multiobjective optimization of composite laminates using a GA
Institut FEMTO-ST, UMR 6174, 24 rue de l'épitaphe, 25000 Besançon, France
2 Currently visiting Aerospace Structures, Faculty of Aerospace Engineering, TU Delft, The Netherlands
3 ONERA, DMSC 29 avenue de la division Leclerc, 92322 Chatillon Cedex, France
Corresponding author: firstname.lastname@example.org
Accepted: 28 March 2008
In this article, complexities related to the multicriteria (multiobjective) optimization of laminated composite structures subjected to technological constraints will be presented. So, various technological constraints will be presented and a strategy of handling each constraint (in order to use the multi-objective optimization tools based on genetic algorithms) will be also introduced.
© ASMDO, EDP Sciences, 2008
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