Multiobjective wing design using genetic algorithms and fuzzy logic
Abstract The designer frequently faces problems in which the project depends on many parameters and the final solution must be evaluated according to several optimization objectives. This may be the case for the aeroelastic and aeromechanical design of lifting surfaces. The aim of the present paper...
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Veröffentlicht in: | Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2004-04, Vol.218 (2), p.133-145 |
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Format: | Artikel |
Sprache: | eng |
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