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A technique for the multiobjective optimisation of laminated composite structures using genetic algorithms and finite element analysis

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dc.contributor.author Walker, Mark
dc.contributor.author Smith, Ryan E.
dc.date.accessioned 2011-08-01T06:10:45Z
dc.date.available 2011-08-01T06:10:45Z
dc.date.issued 2003
dc.identifier.uri http://hdl.handle.net/10321/630
dc.description Originally published in: Composite Structures, Vol. 62, No. 1, 2003. en_US
dc.description.abstract A methodology for using genetic algorithms with the finite element method to minimise a weighted sum of the mass and deflection of fibre reinforced structures with several design variables is described. The design constraint implemented is based on the Tsai–Wu failure criterion. Symmetrically laminated composite rectangular plates with eight layers are used to demonstrate the technique. Thus, the four fibre orientations and laminae thicknesses are to be determined optimally by defining a design index comprising a weighted average of the objective functions and determining the minimum. In addition, the fibre orientations and layer thicknesses must be selected from a set of discrete values. Results are presented for different load distributions, and various combinations of clamped, simply supported and free boundary conditions. The effect of aspect ratio on the results is also investigated. en_US
dc.format.extent pp. 123-128 (6 p.) en_US
dc.language.iso en en_US
dc.publisher Elsevier en_US
dc.rights The electronic version of the article published in Composite Structures 2003, 62(1): 123-128 © 2003 copyright Elsevier. Composite Structures available online at: http://www.sciencedirect.com/science/article/pii/S0263822303000989 en_US
dc.title A technique for the multiobjective optimisation of laminated composite structures using genetic algorithms and finite element analysis en_US
dc.type Article en_US
dc.publisher.uri http://dx.doi.org/10.1016/S0263-8223(03)00098-9 en_US


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