Multi-objective multi-laminate design and optimization of a Carbon Fibre Composite wing torsion box using evolutionary algorithm

The present study aims to minimize the weight of multi-laminate aerospace structures by a classical Genetic Algorithm (GA) interfaced with a CAE solver. The structural weight minimization is a multi-objective optimization problem subjected to fulfilling of strength and stiffness design requirements...

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Veröffentlicht in:	Composite structures Jg. 185; S. 132 - 147
Hauptverfasser:	Shrivastava, Sachin, Mohite, P.M., Yadav, Tarun, Malagaudanavar, Appasaheb
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Elsevier Ltd 01.02.2018
Schlagworte:	Carbon Fibre Composites Genetic algorithms Multi-objective optimization Python-scripting Smart tailoring Wing torsion box Python-scripting Multi-objective optimization Smart tailoring Wing torsion box Carbon Fibre Composites Genetic algorithms
ISSN:	0263-8223, 1879-1085
Online-Zugang:	Volltext
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