| Citation: | XIANG Hong-hui, HOU Min-jie, LIU Zhi-gang. Correlative analysis of performance experimental data of axial flow fans/compressors based on statistical characteristic[J]. Journal of Aerospace Power, 2014, 29(1): 146-152. doi: 10.13224/j.cnki.jasp.2014.01.019 |
| [1] |
Steinke R J.A compute code for predicting multi-stage axial-flow compressor performance by a meanline stage stacking method[R].NASA TP-2020, 1982.
|
| [2] |
程荣辉, 雷丕霓, 刘波, 等.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(6):955-960. CHENG Ronghui, LEI Pini, LIU Bo, et al.A two dimension numerical method for multi-stage axial compressor performance in engineering applications[J].Journal of Aerospace Power, 2007, 22(6):955-960.(in Chinese)
|
| [3] |
Mansour M, Hingorani S, Dong Y.A new multistage axial compressor designed with the APNASA multistage CFD code:Part 1 code calibration[R].ASME Paper 2001-GT-0349, 2001.
|
| [4] |
Dong Y, Mansour M, Hingorani S, et al.A new multistage axial compressor designed with the APNASA multistage CFD code:Part 2 application to a new compressor design[R].ASME Paper 2001-GT-350, 2001.
|
| [5] |
Johnsen I A, Ullock R O.Aerodynamic design of axial flow compressors[R].NASA N65-23345, 1965.
|
| [6] |
Wassell A B.Reynolds number effects in axial compressors[R].ASME Paper WA/GT-2, 1967.
|
| [7] |
Kurzke J, Riegler C.A new compressor map scaling procedure for preliminary conceptional design of gas turbines[R].ASME Paper 2000-GT-0006, 2000.
|
| [8] |
Kong C D, Ki J Y.A new scaling method for component maps of gas turbine using system identification[J].Journal of Engineering for Gas Turbines Power, 2003, 125(4):979-985.
|
| [9] |
Nezym V Y, Polupan G P.A new statistical-based correlation for the compressor tandem cascade parameters effects on the loss coefficient[R].ASME Paper GT2007-27245, 2007.
|
| [10] |
Drummond C, Davison C R.Capturing the shape variance in gas turbine compressor maps[R].ASME Paper GT2009-60141, 2009.
|
| [11] |
Cravero C, Macelloni P.A new model for the prediction of compressor performance maps.International Society for Air Breathing Engines, ISABE-2009-1133, 2009.
|
| [12] |
Kurzke J.Correlations hidden in compressor maps[R].ASME Paper GT2011-45519, 2011.
|
| [13] |
XIANG Honghui, REN Minglin.Discussion of several questions with efficiency assessment in axial flow compressor experiment[R].Japan Society for Aeronautical and Space Sciences, JSASS-2009-5537, 2009.
|
| [14] |
向宏辉, 葛宁, 任铭林.基于试验数据的轴流压气机喘振边界经验预估方法[J].燃气轮机技术, 2011, 24(1):40-44. XIANG Honghui, GE Ning, REN Minglin.Empirical prediction method of the surge line of axial flow compressors based on statistical experimental data[J].Gas Turbine Technology, 2011, 24(1):40-44.(in Chinese)
|
| [15] |
向宏辉, 侯敏杰, 刘志刚.一种实现轴流压气机试验特性关联的经验方法[J].航空动力学报, 2013, 28(7):1517-1525. XIANG Honghui, HOU Minjie, LIU Zhigang.Experiential method for realizing correlation of experimental characteristics of axial flow compressors[J].Journal of Aerospace Power, 2013, 28(7):1517-1525.(in Chinese)
|