STIFFNESS OPTIMIZATION OF LAMINATES BASED ON A MODIFIED PARALLEL SIMULATED ANNEALING METHOD

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JAVIDRAD F.; NOURI R.

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Paper Information

Journal: JOURNAL OF AERONAUTICAL ENGINEERING (JOAE) Year:2011 | Volume:13 | Issue:1 Page(s): 87-97

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Information Journal Paper

Title

STIFFNESS OPTIMIZATION OF LAMINATES BASED ON A MODIFIED PARALLEL SIMULATED ANNEALING METHOD

Author(s)

JAVIDRAD F. | NOURI R. | Issue Writer Certificate

Keywords

SIMULATED ANNEALINGQ2

PARALLELISMQ2

ADAPTIVE COOLING SCHEDULEQ2

LAMINATESQ2

Abstract

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.

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APA: Copy

JAVIDRAD, F., & NOURI, R.. (2011). STIFFNESS OPTIMIZATION OF LAMINATES BASED ON A MODIFIED PARALLEL SIMULATED ANNEALING METHOD. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), 13(1), 87-97. SID. https://sid.ir/paper/173108/en

Vancouver: Copy

JAVIDRAD F., NOURI R.. STIFFNESS OPTIMIZATION OF LAMINATES BASED ON A MODIFIED PARALLEL SIMULATED ANNEALING METHOD. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE)[Internet]. 2011;13(1):87-97. Available from: https://sid.ir/paper/173108/en

IEEE: Copy

F. JAVIDRAD, and R. NOURI, “STIFFNESS OPTIMIZATION OF LAMINATES BASED ON A MODIFIED PARALLEL SIMULATED ANNEALING METHOD,” JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), vol. 13, no. 1, pp. 87–97, 2011, [Online]. Available: https://sid.ir/paper/173108/en

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