• DocumentCode
    3317089
  • Title

    Multi-objective optimization for aerodynamic designs by using ARMOGAs

  • Author

    Obayashi, Shigeru ; Sasaki, Daisuke

  • Author_Institution
    Inst. of Fluid Sci., Tohoku Univ., Japan
  • fYear
    2004
  • fDate
    20-22 July 2004
  • Firstpage
    396
  • Lastpage
    403
  • Abstract
    Global trade-offs for aerodynamic design of supersonic transport (SST) have been investigated by multiobjective evolutionary algorithms (MOEAs). The objectives are to reduce both drag and sonic boom to make next-generation SST more feasible. Adaptive range multiobjective genetic algorithms (ARMOGAs) are utilized for the efficient search. The trade-offs are analysed by self-organizing map (SOM), which provides a topology preserving mapping from the high dimensional space to two dimensions. ARMOGAs and SOM can be good design tools to conduct aerodynamic design optimizations and analyse the results.
  • Keywords
    aerodynamics; aerospace computing; aircraft; computational fluid dynamics; genetic algorithms; self-organising feature maps; adaptive range multiobjective genetic algorithms; aerodynamic designs; drag reduction; multiobjective evolutionary algorithms; multiobjective optimization; self-organizing map; sonic boom reduction; supersonic transport; Aerodynamics; Algorithm design and analysis; Computational fluid dynamics; Design optimization; Drag; Encoding; Evolutionary computation; Genetic algorithms; Sampling methods; Topology;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    High Performance Computing and Grid in Asia Pacific Region, 2004. Proceedings. Seventh International Conference on
  • Print_ISBN
    0-7695-2138-X
  • Type

    conf

  • DOI
    10.1109/HPCASIA.2004.1324064
  • Filename
    1324064