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基于参数化的涡轮叶片三维气动优化仿真
引用本文:马洪波,朱剑,席平.基于参数化的涡轮叶片三维气动优化仿真[J].计算机仿真,2008,25(10).
作者姓名:马洪波  朱剑  席平
作者单位:1. 北京航空航天大学航空科学与工程学院,北京,100083
2. 北京航空航天大学机械工程及自动化学院,北京,100083
摘    要:为了提高涡轮叶片的设计效率,在分析已有涡轮叶片截面线参数化造型技术优缺点的基础上,基于B样条曲线实现了涡轮叶片截面线的参数化造型和参数化修改,并编写了叶片造型程序,实现了叶片流场模型的自动化生成.以某型号涡轮叶片为例,对其进行三维流场数值模拟,然后采用遗传算法和序列二次规划法算法的组合,以涡轮的气动效率为目标函数,对涡轮叶片进行了气动优化.算例结果表明文中所建立的涡轮叶片自动优化设计体系是可行的.

关 键 词:涡轮叶片  参数化设计  样条  优化仿真  效率

Aerodynamic 3D Optimization Simulation of Turbine Blade Based on Parametric Design
MA Hong-bo,ZHU Jian,XI Ping.Aerodynamic 3D Optimization Simulation of Turbine Blade Based on Parametric Design[J].Computer Simulation,2008,25(10).
Authors:MA Hong-bo  ZHU Jian  XI Ping
Affiliation:MA Hong-bo1,ZHU Jian2,XI Ping2(1.School of Aeronautic Science , Eengineering,Beihang University,Beijing 100083,China,2.School of Mechanical Engineering , Automation,China)
Abstract:To improve the design efficiency of turbine blade, based on analyzing the advantages and disadvantages of the existing parameterized modeling of the turbine blade section curve, the paper actualized the parameterized modeling and parameterized modification of the section curve. The blade modeling was programmed and the flow flied calculation of blades was automatically modeled.3D flow flied of blades was simulated, then aerodynamic optimization was carried out using the GA and SQA algorithms by taking the a...
Keywords:Turbine blade  Parametric design  Spline  Optimization simulation  Efficiency  
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