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一种基于数值计算的轴流压气机旋转失速稳定性模型——之二:简化模型及应用
引用本文:侯睿炜,孙晓峰.一种基于数值计算的轴流压气机旋转失速稳定性模型——之二:简化模型及应用[J].航空动力学报,2009,24(12):2735-2740.
作者姓名:侯睿炜  孙晓峰
作者单位:北京航空航天大学能源与动力工程学院,北京,100191
摘    要:提出了一个基于直接数值计算结果基础上的旋转失速线性稳定性模型,描述了如何从基本的Navier-Stokes方程出发,把轴流压气机流动稳定性问题转化为一个特征值问题的基本理论框架,对压气机不稳定边界的判断通过计算和检验特征值的方式来实现,给出了有限差分法和基于Gauss-Lobatto节点的谱配置方法两种数值离散的方式,并分析了这两种离散方式的收敛特性.

关 键 词:轴流压气机  旋转失速  稳定性  特征值  有限差分法  谱方法
收稿时间:9/3/2009 12:00:00 AM
修稿时间:2009/11/12 0:00:00

A linear stability model of rotating stall based on direct numerical techniques:part II- a simplified model and its applications
HOU Rui-wei and SUN Xiao-feng.A linear stability model of rotating stall based on direct numerical techniques:part II- a simplified model and its applications[J].Journal of Aerospace Power,2009,24(12):2735-2740.
Authors:HOU Rui-wei and SUN Xiao-feng
Institution:Fluid and Acoustic Engineering Laboratory of Beijing University of Aeronautics and Astronautics
Abstract:A two-dimensional linear stability model was presented,which can be used to estimate the inception point of rotating stall in axial flow compressors by solving the eigenvalues,the effects of the blade rows in compressors on the flow field have been modeled by body force source terms in the momentum equations.Two methods,finite difference and spectral collocation methods,have been used to discretize the eigenvalue equations.The validations of model have been performed in two different cases,and the results show that the simplified model is able to predict the stall onset point of low-speed axial compressors.
Keywords:axial compressor  rotating stall  stability  eigenvalue  finite difference method  spectral method
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