大小叶片压气机级的计算与实验校验

推进技术 ›› 2014, Vol. 35 ›› Issue (3): 335-340.

大小叶片压气机级的计算与实验校验

王洪伟¹,刘涛¹,宁方飞²

北京航空航天大学能源与动力工程学院/航空发动机气动热力国家级重点实验室,北京 100191;北京航空航天大学能源与动力工程学院/航空发动机气动热力国家级重点实验室,北京 100191;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

发布日期:2021-08-15
作者简介:王洪伟(1973—),博士,讲师,研究领域为叶轮机械气动热力学。 E-mail:wanghw@buaa.edu.cn

Numerical Simulation and Experimental Validation of a Compressor Stage with Splittered Rotor

National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;Aero-Engine Numerical Simulation Research Center, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics,Beijing 100191, China

Published:2021-08-15

摘要/Abstract

摘要： 为了考察用于压气机设计的三维计算软件的准确性,对一个低速大尺寸的单级大小叶片轴流压气机进行了计算与流动测量,基于可压缩流动,并在流动细节的层次上全面地考察了计算程序的准确性。结果表明:所用的计算程序对压气机设计点的计算较为准确,流量和压比的准确度可达1%,但对失速裕度的预估能力不足。计算程序对于内部流动细节,尤其是二次流动的模拟不够好,当压气机工作于非设计工况时,这些流动细节计算的不准确会导致整体性能上较大的偏差。 

关键词: 低速大尺寸模拟;实验验证;数值模拟;压气机特性;流动分析 

Abstract: In order to validate the accuracy of a 3-D computation code used for compressor design, a low-speed large-scale single-stage axial flow compressor with splittered rotor was computed and detailed flow inside the compressor was measured. To have a comprehensive examination to the computation code, the experiment was performed based on compressible flow, and the internal flow was documented in detail. It is concluded from the comparison that the computation code is capable of simulating the nominal characteristics of the compressor with accuracy of 1% for both the flow rate and pressure ratio, while incapable of forecasting stall margin. On the other hand, the computational code is incompetent for complex flow simulation, especially for the secondary flow. This makes the characteristics predicted by the computation code also questionable, especially for off-design circumstance. 

Key words: Low-speed large-scale simulation; Experimental validation; Numerical simulation; Compressor characteristics; Flow analysis

王洪伟,刘涛,宁方飞. 大小叶片压气机级的计算与实验校验[J]. 推进技术, 2014, 35(3): 335-340.

WANG Hong-wei¹, LIU Tao¹, NING Fang-fei². Numerical Simulation and Experimental Validation of a Compressor Stage with Splittered Rotor[J]. Journal of Propulsion Technology, 2014, 35(3): 335-340.

参考文献

[1] Wennerstrom A J, Frost G R.Design of a Rotor Incorporating Splitter Vanes for a High Pressure Ratio Supersonic Axial Compressor Stage[C].Ohio:Patterson AFB, Aerospace Research Labs Wright, 1974.
[2] Wennerstrom A J, Buzzell W A, Derose R D.Test of a Supersonic Axial Compressor Stage Incorporating Splitter Vanes in the Rotor[C].Ohio:Patterson AFB,Aerospace Research Labs Wright, 1975.
[3] Tzuoo K L.Optimization of a Highly Loaded Axial Splittered Rotor Design[C].Revue:Francaise de Mécanique,1992.
[4] Opdyke C E.Integrated High Performance Turbine Engine Technology (IHPTET)[J].Gas Turbine Forecast,2006,0(3):1-8.
[5] 严明, 陈懋章.大小叶片轴流压气机转子流动特性分析[J].推进技术,2002,3(4):280-282.(YAN Min, CHEN Mao-zhang.Flow Performance Analysis in an Axial Compressor Rotor with Splitter[J].Journal of Propulsion Technology, 2002,3(4):280-282.)
[6] 张永新, 邹正平, 严明, 等.单级大小叶片轴流压气机流动分析[J].航空动力学报,2004,9(1).
[7] 李海鹏.轴流大小叶片流动机理的数值模拟研究[D].北京:北京航空航天大学, 2007.
[8] 李海鹏, 刘火星, 蒋浩康.单级轴流大小叶片压气机非定常流场数值研究[J].航空动力学报,2006,1(6):423-430.
[9] 王洪伟,蒋浩康,陈懋章.大小叶片压气机平面叶栅试验研究[J].工程热物理学报,2006,增刊(1):113-117
[10] Casey M, Innotec S.Best Practice Advice for CFD in Turbomachinery Design[J].QNET CFD Network Newsletter, 2003,2(3):35-37.
[11] Molinari M, Dawes W N.Review of Evolution of Compressor Design Process and Future Perspectives[J].Mechanical Engineering Science, 2006,0(C):761-771.
[12] Horlock J H, Denton J D.A Review of Some Early Design Practice Using Computational Fluid Dynamics and a Current Perspective[J].Journal of Turbomachinery, 2005,7(1):5-13.
[13] Denton J D.An Improved Time-marching Method for Turbomachinery Flow Calculation[J].Journal of Engineering for Power, 1983,5:514-524.
[14] Denton J D.The Calculation of Three-Dimensional Viscous Flow Through Multistage Turbomachines[J].Journal of Turbomachinery, 1992,4(1):18-26.
[15] 蒋浩康, 王洪伟, 李雨春.圆柱单孔高频压力探针[P].中国专利:200410028908.X,2009-07-01.
[16] 蒋浩康, 王洪伟, 李雨春.锥面四孔高频压力探针[P].中国专利:200410028909.X,2009-07-01.
[17] 王洪伟.高负荷轴流压气机级的试验与数值研究[D].北京:北京航空航天大学, 2010.
[18] Denton J D, Xu L.CFD for Turbomachinery Aerodynamic Design[C].London:IMECHE Grand review of CFD, 2002.