| Citation: | HU Jiang-feng, ZHU Xiao-cheng, DU Zhao-hui. Numerical method of transonic axial compressor performance prediction[J]. Journal of Aerospace Power, 2011, 26(1): 122-127.
|
| [1] |
Boyer K M,O’Brien W F.An improved streamline curvature approach for off-design analysis of transonic axial compression systems[J].Journal of Turbomachinery,2003,125(3):475-481.
|
| [2] |
Johnsen I A,Bullock R O.Aerodynamic design of axial-flow compressor .NASA-SP-36,1965.
|
| [3] |
Cetin M,Ucer A S,Hirsch C,et al.Application of modified loss and deviation correlations to transonic axial compressors .AGRAD-R-745,1987.
|
| [4] |
Pachidis V.An iterative method for blade profile loss model adaptation using streamline curvature[J].Journal of Engineering of Gas Turbines and Power,2008,130(1):1-8.
|
| [5] |
Aungier R H.Axial-flow compressor:a strategy for aerodynamic design and analysis[M].New York:ASME Press,2003.
|
| [6] |
Templalexis I,Pilidis P,Pachidis V,et al.Development of a 2-D compressor streamline curvature code .ASME GT2006-90867,2006.
|
| [7] |
Ali M,Ali H B.Performance prediction modeling of axial-flow compressor at design and off-design conditons .ASME GT2008-50550,2008.
|
| [8] |
Miller G R,Lewis G W,Hartmann M J.Shock losses in transonic compressor blade rows[J].Journal of Engineering of Power,1961,83:235-242
|
| [9] |
杜文海,吴虎,黄健.跨声速多级轴流压气机非设计性能预测[J].航空动力学报,2007,22(9):1481-1486. DU Wenhai,WU Hu,HUANG Jian.Off-design performance prediction of multi-stage transonic axial compressor[J].Journal of Aerospace Power,2007,22(9):1481-1486.(in Chinese)
|
| [10] |
程荣辉,雷丕霓,周盛.一种工程实用的多级轴流压气机特性二维数值计算方法[J].航空动力学报,2007,22(9):955-960. CHENG Ronghui,LEI Pini,ZHOU Sheng.A two-dimension numerical method for multi-stage axial compressor performance in engineer applications[J].Journal of Aerospace Power,2007,22(9):955-960.(in Chinese)
|
| [11] |
赵勇,胡骏,屠宝锋,等.多级轴流风扇/压气机非设计点性能计算方法[J].推进技术,2008,29(2):119-224. ZHAO Yong,HU Jun,TU Baofeng,et al.Calculation of multistage axial fan/compressor off-design performance[J].Journal of Propulsion Technology,2008,29(2):119-224.(in Chinese)
|
| [12] |
Royce D M,Lonnie R.Performance of single stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26,respectively,and with design pressure ratio of 2.05 .NASA-TP-1659,1980.
|
DownLoad: