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静止叶栅三维粘性数值模拟
引用本文:严明,彭泽琰. 静止叶栅三维粘性数值模拟[J]. 航空动力学报, 1999, 14(4): 397-400
作者姓名:严明  彭泽琰
作者单位:北京航空航天大学
摘    要:应用N- S方程压力修正算法和k- ε两方程湍流模型,对端弯叶片和基准(无端弯)叶片的平面叶栅进行了三维粘性数值模拟。在采用简单交错网格的情况下,通过对计算控制体通量的速度进行修正的方法解决了N- S方程压力修法算中遇到的压力场和速度场呈锯齿状分布的问题。用实验测量值对本数值模拟方法的精度和可靠性进行了检验

关 键 词:叶栅   流场   数值模拟
收稿时间:1998-11-01
修稿时间:1999-03-01

A 3-D VISCOUS NUMERICAL SIMULATION FOR STATIC COMPRESSOR CASCADE
Yan Ming and Peng Zeyan. A 3-D VISCOUS NUMERICAL SIMULATION FOR STATIC COMPRESSOR CASCADE[J]. Journal of Aerospace Power, 1999, 14(4): 397-400
Authors:Yan Ming and Peng Zeyan
Affiliation:4th Dept.Beijing University of Aeronautics and Astronautics,Beijing 100083
Abstract:A 3-D viscous numerical simulation was completed for the plane cascade flow fields of end-bend and original blade with the helps of pressure-based method of N-S equations and a K-ε two equations model.In the case of using simple stagger grid,by the way of velocity modification for calculating flux of a control volume,the well-known problem of checkerboard distribution of pressure and velocity fields in the pressure-based method is well settled.The accuracy and reliability of this numerical simulation are verified with the experimental data. 
Keywords:Cascades Flow fields Numerical models
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