Volume 22 Issue 1
Jan.  2007
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SHU Xin-wei, GU Chuan-gang, YANG Bo, WANG Tong. Aerodynamic optimization for cascade blade based onNiche GAs and RANS equation[J]. Journal of Aerospace Power, 2007, 22(1): 48-53.
Citation: SHU Xin-wei, GU Chuan-gang, YANG Bo, WANG Tong. Aerodynamic optimization for cascade blade based onNiche GAs and RANS equation[J]. Journal of Aerospace Power, 2007, 22(1): 48-53.
shu

Aerodynamic optimization for cascade blade based onNiche GAs and RANS equation

  • School of Mechanical Engineering, Shanghai Jiaotong University, Shanghai 200030, China

  • Received Date: 2005-12-27
  • Rev Recd Date: 2006-04-06
  • Publish Date: 2007-01-28
    Abstract
  • A global optimization method for cascade blade based on Niche GAs(Niche genetic algorithms) coupled with RANS(Reynolds-Averaged Navier-Stokes) equation has been presented.In order to meet the search theory of GAs and the aerodynamic performances of cascade blade,Bezier curve is adopted to parameterize the cascade blade profile in this method,and a fitness function pertaining to optimization is designed.The design variables are the control points' ordinates of Bezier curve representing the cascade blade profile;the object function is the maximum lift-drag ratio of the cascade;the constraint conditions take account of the leading and trailing edge metal angle,and the strength and aerodynamic performers of cascade blade;and the treatment method of the constraint conditions is the flexible penalty function.The lift-drag ratio of optimized cascade is 8.3 percent higher than that of the initial one.

     

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    • References(8)
  • [1]
    刘高联.平面叶栅气动设计的最优化理论[J].力学学报,1980,4:337-346.LIU Gaolian.Optimum theory of the cascade aerodynamic design[J].Chinese Journal of Theoretical and Applied Mechanics,1980,4:337-346.
    [2]
    Shelton M L,Gregory B A.Optimization of a transonic turbine airfoil using artificial intelligence,CFD and cascade testing[R].ASME Paper 1993-GT-161.
    [3]
    Pierret S,Van den Braembussche R A.Turbomachinery blade design using a navier-stokes solver and artificial neural network[J].ASME Journal of Turbomachinery,1999,121:326-332.
    [4]
    Reuther J,Jameson A.Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation[R].AIAA Paper 1996-0094.
    [5]
    Burguburu S,Toussaint C,et al.Numerical optimization of turbomachinery bladings[J].ASME Journal of Turbomachinery,2004,126:91-100.
    [6]
    Oksuz O,Akmandor I S.Aerodynamic optimization of turbomachinery cascades using euler/boundary-layer coupled genetic algorithms[R].AIAA Paper 2001-2577
    [7]
    Spalart P R,Allmaras S R.A one-equation turbulence model for aerodynamic flows[R].AIAA Paper 1992-0439.
    [8]
    Goldberg D E,Richardson J.Genetic algorithms with sharing for multimodal function optimization[R].Proc.2nd Int.Conf.Genetic Algorithms and their Applications,1987,41-49.
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