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轴流压缩系统动态失速的简化模型
引用本文:胡骏.轴流压缩系统动态失速的简化模型[J].航空学报,1997,18(2):207-209.
作者姓名:胡骏
作者单位:南京航空航天大学动力工程系
摘    要: 在原Moore-Greitzer模型的基础上,发展了一个描述轴流压缩系统动态失速过程的一阶非线性模型。该模型耦合了旋转失速和喘振,并考虑了旋转扰动波中高阶谐波分量的影响,可用于详细分析旋转失速/喘振的动态特性、由失速状态退出的恢复特性,及系统参数的影响等。

关 键 词:压缩系统  旋转失速  喘振  恢复特性  

NEW SIMPLIFIED MODEL OF POST STALL TRANSIENTS IN AXIAL COMPRESSION SYSTEMS
Hu Jun.NEW SIMPLIFIED MODEL OF POST STALL TRANSIENTS IN AXIAL COMPRESSION SYSTEMS[J].Acta Aeronautica et Astronautica Sinica,1997,18(2):207-209.
Authors:Hu Jun
Institution:Power Engineering Department, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016
Abstract:Based on the theory developed by Moore and Greitzer, a new simplifying approximation, which takes into account the influence of higher harmonics of rotating waves, is proposed to get a simplified model of post stall transients in axial compression systems. This model consists of a set of three simultaneous nonlinear first order partial differential equations.It is shown that the further investigations of post stall behavior for different response modes of instabilities (rotating stall and/or surge), recoverability from rotating stall or surge, and the effect of compression system parameters on them can be carried out by this model.
Keywords:compression system  rotating stall  surge  recoverability  
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