Stacking sequence design of composite laminates for maximum strength using genetic algorithms

By Jaesung Park, Jungho Hwang, Chang-Woo Lee, W. Hwang. 2001

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Optimum design of composite laminates for maximum buckling load capacity using simulated annealing (2005, methodology): “[3] used a GA for the optimal design of composite laminates which comprises four plies subject to various in-plane loading conditions.”
MULTI-OBJECTIVE OPTIMIZATION OF FIBER REINFORCED COMPOSITE LAMINATES FOR STRENGTH, STIFFNESS AND MINIMAL MASS (2006, methodology): “[9] analyzed symmetric composite laminates using a shear deformation theory and the Tsai–Hill failure criterion to obtain optimal designs of symmetric composite laminates subject to various loading and boundary conditions.”
Optimum stacking sequence design of composite materials Part I: Constant stiffness design (2009, methodology): “GA has been used for several objective functions, such as strength [61,63], buckling loads [61,64–70], dimensional stability [71], strain energy absorption [72], weight (either as a constraint or as an objective to be minimized) [73,52,74–77], bending/twisting coupling [67], stiffness [72,78], funda”