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预处理方法在叶轮机械三维数值模拟中的应用
引用本文:严明,赵秋颖,梁磊.预处理方法在叶轮机械三维数值模拟中的应用[J].航空动力学报,2007,22(1):41-47.
作者姓名:严明  赵秋颖  梁磊
作者单位:1.北京航空航天大学 航空发动机气动热力重点实验室, 北京, 100083
摘    要:应用预处理方法求解三维可压缩流动Navier-Stokes方程, 发展了一种适用于叶轮机械的既可以求解跨声速流动也可以求解不可压流动的数值模拟方法, 对NASA Rotor67和北航低速大尺寸压气机算例进行了计算, 计算结果与实验数据相吻合, 表明本文采用的预处理方法具有较大的工程实用性. 

关 键 词:航空、航天推进系统    叶轮机械    预处理    Navier-Stokes方程
文章编号:1000-8055(2007)01-0041-07
收稿时间:2005/12/29 0:00:00
修稿时间:2005年12月29

Appl ication of preconditioning method in 3D numericalsimulation of turbomachinery
YAN Ming,ZHAO Qiu-ying and LIANG Lei.Appl ication of preconditioning method in 3D numericalsimulation of turbomachinery[J].Journal of Aerospace Power,2007,22(1):41-47.
Authors:YAN Ming  ZHAO Qiu-ying and LIANG Lei
Institution:1.National Key Laboratory on Aero-Engines, Beijing University of Aeronautics and Astronautics, Beijing 100083, China2.School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:A preconditioning technique for solving 3-D compressible Navier-Stokes equations is developed to simulate both transonic and incompressible flows in turbomachinery.Computations over NASA Rotor 67 and a low-speed large-scale compressor stage in Beijing University of Aeronautics and Astronautics were performed and the results are in accordance with experimental data,it shows that the method presented is practical for engineering usage.
Keywords:aerospace propulsion system  turbomachinery  preconditioning  Navier-Stokes equations
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