Simulated annealing is one the most popular methods that provides a means for optimization of problems with both continuous and discrete variables. The method is basically a Monte-Carlo random search technique in which movement from a local extremum is heuristically possible. In this paper, an approach to the design of laminates based on a modified discrete-variables parallel simulated annealing method is presented. The eight effective elastic moduli and the weight of the laminate are used to develop a cost function that its minimization gives a proper lay-up to be compatible with the required elastic effective moduli and a minimum weight. A parallel simulated annealing procedure in conjunction with a novel adaptive cooling schedule is introduced to speed up the algorithm. Studies show that the introduced modifications are also statistically effective in increasing the solution quality.
Javidrad,F. and Nouri,R. (2011). Stiffness Optimization of Laminates based on a modified Parallel Simulated Annealing method. Journal of Aeronautical Engineering, 13(1), 87-97.
MLA
Javidrad,F. , and Nouri,R. . "Stiffness Optimization of Laminates based on a modified Parallel Simulated Annealing method", Journal of Aeronautical Engineering, 13, 1, 2011, 87-97.
HARVARD
Javidrad F., Nouri R. (2011). 'Stiffness Optimization of Laminates based on a modified Parallel Simulated Annealing method', Journal of Aeronautical Engineering, 13(1), pp. 87-97.
CHICAGO
F. Javidrad and R. Nouri, "Stiffness Optimization of Laminates based on a modified Parallel Simulated Annealing method," Journal of Aeronautical Engineering, 13 1 (2011): 87-97,
VANCOUVER
Javidrad F., Nouri R. Stiffness Optimization of Laminates based on a modified Parallel Simulated Annealing method. JoAE, 2011; 13(1): 87-97.