• DocumentCode
    348730
  • 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
  • Volume
    4
  • fYear
    1999
  • fDate
    1999
  • Firstpage
    475
  • 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;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems, Man, and Cybernetics, 1999. IEEE SMC '99 Conference Proceedings. 1999 IEEE International Conference on
  • Conference_Location
    Tokyo
  • ISSN
    1062-922X
  • Print_ISBN
    0-7803-5731-0
  • Type

    conf

  • DOI
    10.1109/ICSMC.1999.812450
  • Filename
    812450