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某小型涡喷发动机二维数值仿真
引用本文:曹志鹏,刘大响,桂幸民,邹正平,岳明.某小型涡喷发动机二维数值仿真[J].航空动力学报,2009,24(2):439-444.
作者姓名:曹志鹏  刘大响  桂幸民  邹正平  岳明
作者单位:北京航空航天大学能源与动力工程学院航空发动机数值仿真研究中心,北京,100191
摘    要:整机二维仿真模型由带有粘性项的二维欧拉方程,燃烧模型和损失模型构成.利用任意曲线坐标系来适应复杂几何边界计算,采用隐式高阶精度Godunov格式求解非定常欧拉方程,能够自动捕捉激波,数值稳定性高.计算的总性能参数与设计值对比显示:单部件的仿真精度高于整机,涡轮仿真精度高于压气机.子午平面上的计算结果分析表明:离心压气机出口处的分离流动、燃烧室掺混孔的简化对总性能参数计算结果影响较大.

关 键 词:整机二维仿真  欧拉方程  损失模型
收稿时间:2008/1/16 0:00:00
修稿时间:2008/7/13 0:00:00

Two dimensional numerical simulation of small turbojet engine
CAO Zhi-peng,LIU Da-xiang,GUI Xing-min,ZOU Zheng-ping and YUE Ming.Two dimensional numerical simulation of small turbojet engine[J].Journal of Aerospace Power,2009,24(2):439-444.
Authors:CAO Zhi-peng  LIU Da-xiang  GUI Xing-min  ZOU Zheng-ping and YUE Ming
Institution:Aeroengine Numerical Simulation Research Center;School of Jet Propulsion;Beijing University of Aeronautics and Astronautics;Beijing 100191;China
Abstract:two-dimensional Euler equation,combustion model and loss calculation methods were used to establish the numerical simulation model of engine.A body fitted coordinate system is used to adapt the complex geometry boundary.Unsteady Euler equation was solved by implicit high order Godunov scheme,which had the characteristic of shock capturing and good numerical stability.The data comparisons of calculation and design showed: the components simulation precision was higher than that of whole engine,the turbine si...
Keywords:two-dimensional numerical simulation of whole engine  Euler equation  loss model  
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