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. & 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., & 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
Javidrad, F. & Nouri, R., "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 (In Persian).