• DocumentCode
    2069894
  • Title

    Aerodynamic optimization designing of airfoil based on Isight

  • Author

    Wang, Wei ; Mo, Rong ; Chang, Zhiyong ; Sun, Huibin

  • Author_Institution
    Key Lab. of Contemporary Design & Integrated Manu.Tech., Northwestern Polytech. Univ., Xi´´an, China
  • Volume
    1
  • fYear
    2010
  • fDate
    10-12 Dec. 2010
  • Firstpage
    262
  • Lastpage
    266
  • Abstract
    In order to improving the designing efficiency and achieving automation of airfoil optimization designing, A method which combined the airfoil parametric modeling software, the CFD software with Isight platform was presented, it was used to optimize the airfoil to ameliorate its aerodynamic performance. During the process of optimization designing, first, we adopted the design of experiment (DOE) method to search the designing space, achieved the optimal initialization design. Then, we adopted Non-dominated Sorting Genetic Algorithm (NSGA-II) to optimize the airfoil, got the optimal airfoil aerodynamic solution. The optimized solution proved that the aerodynamic performance of the airfoil has been significantly improved, which shows the optimization designing method was reasonable and feasible.
  • Keywords
    aerodynamics; aerospace components; computational fluid dynamics; design of experiments; genetic algorithms; CFD software; Isight; aerodynamic optimization design; airfoil parametric modeling software; design of experiment method; non dominated sorting genetic algorithm; Aerodynamics; Computational fluid dynamics; Hypercubes; Sun; Aerodynamic Optimization Designing of Airfoil; Isight Design of Experiment(DOE); Non-dominated Sorting Genetic Algorithm (NSGA-II);
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Progress in Informatics and Computing (PIC), 2010 IEEE International Conference on
  • Conference_Location
    Shanghai
  • Print_ISBN
    978-1-4244-6788-4
  • Type

    conf

  • DOI
    10.1109/PIC.2010.5687451
  • Filename
    5687451