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混合遗传算法及其在叶片自动优化设计中的应用
引用本文:周正贵.混合遗传算法及其在叶片自动优化设计中的应用[J].航空学报,2002,23(6):571-574.
作者姓名:周正贵
作者单位:南京航空航天大学,能源与动力学院,江苏,南京,210016
摘    要: 在遗传算法中 ,采用单纯形法寻优取代变异运算构成混合遗传算法 ,以提高遗传算法局部搜索能力。算例表明混合遗传算法可有效提高搜索效率和对最优解的逼近程度。采用三次多项式和多圆弧方法生成叶型中弧线 ,三次多项式分布叶型厚度 ,对叶型进行参数化。将N S方程正问题流场数值计算与混合遗传算法相结合 ,构成叶轮机械叶型自动优化设计。尝试由气流转角、总压损失和叶型型面面积构成目标函数 ,对压气机叶型进行自动优化设计。

关 键 词:气动优化  叶片设计  压气机  遗传算法  单纯形法  
文章编号:1000-6893(2002)06-0571-04
修稿时间:2001年11月27

COMPOSITE GENETIC ALGORITHM AND ITS APPLICATION TO AUTOMATIC OPTIMIZATION OF TURBOMACHINERY BLADE
ZHOU Zheng,gui.COMPOSITE GENETIC ALGORITHM AND ITS APPLICATION TO AUTOMATIC OPTIMIZATION OF TURBOMACHINERY BLADE[J].Acta Aeronautica et Astronautica Sinica,2002,23(6):571-574.
Authors:ZHOU Zheng  gui
Institution:College of Energy and Power, Nanjing University of Aeronautics and Astronautics, Nanjing 210016,China
Abstract:To improve the locally searching ability of a genetic algorithm, the mutation operation is replaced by the process of searching for an optimum using the simplex method. The examples show that using the composite genetic algorithm can effectively improve the search efficiency and approach degree to the optimal objective. For constructing the blade mean camber lines, a third order polynomial and a multi arc curve is used. The blade thickness is distributed also by another third order polynomial. The composite genetic algorithm is combined with 2DNS flow field calculation, for an automatic optimization design of the turbomachinery blade. It is attempted that constructing an objective function by the flow turning angle, total pressure loss and blade area; then the composite genetic algorithm is used to design a compressor blade.
Keywords:aerodynamic optimization  blade design  compressor  genetic algorithm  simplex method
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