Title :
Wing design using real-coded adaptive range genetic algorithm
Author :
Oyama, A. ; Obayashi, S. ; Nakahashi, K.
Author_Institution :
Dept. of Aeronaut. & Space Eng., Tohoku Univ., Sendai, Japan
Abstract :
Real-coded adaptive range genetic algorithms (ARGAs) have been developed. The real-coded ARGAs possess both advantages of the binary-coded ARGAs and the use of the floating point representation to overcome the problems of having a large search space that requires continuous sampling. First, the efficiency and the robustness of the proposed approach have been demonstrated by using a typical test function. Then the proposed approach has been applied to an aerodynamic airfoil shape optimization problem. The results confirm that the real-coded ARGAs consistently find better solutions than the conventional real-coded GAs do. The design result is considered to be the global optimal and thus ensures the feasibility of the real-coded ARGAs in aerodynamic designs
Keywords :
computational fluid dynamics; flow simulation; genetic algorithms; structural engineering computing; aerodynamic airfoil shape optimization; aerodynamic designs; continuous sampling; floating point representation; large search space; real-coded adaptive range genetic algorithm; wing design; Aerodynamics; Algorithm design and analysis; Biological cells; Computational fluid dynamics; Genetic algorithms; Genetic engineering; Optimization methods; Robustness; Sampling methods; Shape;
Conference_Titel :
Systems, Man, and Cybernetics, 1999. IEEE SMC '99 Conference Proceedings. 1999 IEEE International Conference on
Conference_Location :
Tokyo
Print_ISBN :
0-7803-5731-0
DOI :
10.1109/ICSMC.1999.812450