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轴流叶轮机多排流动模拟的模型方程
引用本文:季路成,郭恩民,孟庆国,周盛. 轴流叶轮机多排流动模拟的模型方程[J]. 航空动力学报, 1997, 12(2): 194-196,222
作者姓名:季路成  郭恩民  孟庆国  周盛
作者单位:北京航空航天大学
摘    要:首次推导出适合于多排流动模拟的模型方程—时均效应N-S方程,并对所提新概念—时均应力、时均能源的建模问题进行了初步探讨,继而给出了多排流动模拟界面气流参数传递的工程处理方法。该模型理论基础严格,具有很好的应用前景。

关 键 词:叶轮机   流场模拟   多级
收稿时间:1996-05-01
修稿时间:1996-07-01

A MODEL EQUATION FOR SIMULATING FLOW-FIELD IN MULTIROW AXIAL TURBOMACHINES
Ji Lucheng,Guo Enmin,Meng Qinguo and Zhou Sheng. A MODEL EQUATION FOR SIMULATING FLOW-FIELD IN MULTIROW AXIAL TURBOMACHINES[J]. Journal of Aerospace Power, 1997, 12(2): 194-196,222
Authors:Ji Lucheng  Guo Enmin  Meng Qinguo  Zhou Sheng
Affiliation:4th Dept.Beijing University of Aeronautics and Astronautics, Beijing 100083
Abstract:In order to simulate the flow-field in multirow turbomachines,a model equation,named Time-averaged Effect Navier-Stokes equation,(hereafter referred to as TENS equation)has been firstly deduced.This TENS equation was obtained from ensemble average and time average processes in succession.As distinguished from Renolds-averaged N-S equation,the TENS equation has time-averaged stresses and time-averaged energy source terms to consider the zero order unsteady effect.As a result,it gives a better engineering method to transmit parameters across the interface of neighbour blade rows.
Keywords:Turbomachines Flow field simulation Multistages  
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