| Citation: | QIN Yuqi, XUE Fei, WANG Qingyong, et al. Comparative study on the stall prediction ability of two/three-dimensional stability models[J]. Journal of Aerospace Power, 2026, 41（2）：20240309 doi: 10.13224/j.cnki.jasp.20240309
|
Accurately predicting compressor instability boundaries to ensure their structural integrity is a major problem faced by compressor designers at home and abroad, taking NASA Rotor 35 rotors and double-row axial flow counter-rotating compressors as the research objects, firstly, the ability of the two-dimensional model to predict the starting point of single-row and multi-row rotors is evaluated. The results show that for the NASA Rotor 35 rotor, the relative error between the stall point flow obtained by the two-dimensional model and the experimental results is 1.87%. For the double-row counter-rotating compressor, the model differed from the Computational Fluid Dynamics results by 5.9%. In order to solve the problem of low accuracy of the two-dimensional model in predicting the stall speed of the rotary compressor, a three-dimensional stall prediction model was constructed based on the volume force model and the prediction model of the propagation velocity of the stall group. The results show that the relative error between the stall flow rate of Rotor 35 predicted by the developed 3D model and the experimental value is 1.97%, and the relative error between the stall flow rate of the rotary compressor and the Computational Fluid Dynamics result is reduced to 2.14%, greatly solves the defect of insufficient estimation ability caused by the use of a large number of geometric and flow field simplification methods in the current model.
| [1] |
STENNING A, KRIEBEL A. Stall propagation in a cascade of aerofoils[J]. ASME, 1958, 80(4): 777-789.
|
| [2] |
FABRI J, SIESTRUNCK R. Rotating stall propagation in an axial flow compressor [J]. Journal of Aerodynamic Science, 1957, 24(11): 805-817.
|
| [3] |
TAKATA H, NAGANO S. Nonlinear analysis of rotating stall[J]. Journal of Engineering for Power, 1972, 94(4): 279-293. doi: 10.1115/1.3445683
|
| [4] |
SEARS W R. Rotating stall in axial compressors[J]. Zeitschrift Für Angewandte Mathematik und Physik ZAMP, 1955, 6(6): 429-455.
|
| [5] |
GREITZER E M. Surge and rotating stall in axial flow compressors: Part Ⅰ theoretical compression system model[J]. Journal of Engineering for Power, 1976, 98(2): 190-198. doi: 10.1115/1.3446138
|
| [6] |
GREITZER E M. Surge and rotating stall in axial flow compressors: Part Ⅱ experimental results and comparison with theory[J]. Journal of Engineering for Power, 1976, 98(2): 199-211. doi: 10.1115/1.3446139
|
| [7] |
MOORE F K. A theory of rotating stall of multistage axial compressors: Part Ⅰ small disturbances[J]. Journal of Engineering for Gas Turbines and Power, 1984, 106(2): 313-320. doi: 10.1115/1.3239565
|
| [8] |
MOORE F K. A theory of rotating stall of multistage axial compressors: Part Ⅲ limit cycles[J]. Journal of Engineering for Gas Turbines and Power, 1984, 106(2): 327-334. doi: 10.1115/1.3239567
|
| [9] |
MOORE F K, GREITZER E M. A theory of post-stall transients in axial compression systems: Part Ⅰ development of equations[J]. Journal of Engineering for Gas Turbines and Power, 1986, 108(1): 68-76. doi: 10.1115/1.3239887
|
| [10] |
GREITZER E M, MOORE F K. A theory of post-stall transients in axial compression systems: Part Ⅱ application[J]. Journal of Engineering for Gas Turbines and Power, 1986, 108(2): 231-239. doi: 10.1115/1.3239893
|
| [11] |
PADUANO J D, EPSTEIN A H, VALAVANI L, et al. Active control of rotating stall in a low-speed axial compressor[J]. Journal of Turbomachinery, 1993, 115(1): 48-56. doi: 10.1115/1.2929217
|
| [12] |
蔡元虎, 王宏基, 唐狄毅, 等. 多级轴流压气机非设计性能及喘振边界的预测[J]. 航空学报, 1985, 6(5): 417-420. CAI Yuanhu, WANG Hongji, TANG Diyi, et al. Prediction of off-design performance and surge margin of multi-stage axial-flow compressors[J]. Acta Aeronautica et Astronautica Sinica, 1985, 6(5): 417-420. (in Chinese
CAI Yuanhu, WANG Hongji, TANG Diyi, et al. Prediction of off-design performance and surge margin of multi-stage axial-flow compressors[J]. Acta Aeronautica et Astronautica Sinica, 1985, 6(5): 417-420. (in Chinese)
|
| [13] |
屠宝锋, 胡骏, 赵勇. 轴流压气机动态失速过程三维计算[J]. 航空动力学报, 2009, 24(7): 1616-1621. TU Baofeng, HU Jun, ZHAO Yong. Three-dimensional numerical research on stall inception in axial compressor[J]. Journal of Aerospace Power, 2009, 24(7): 1616-1621. (in Chinese doi: 10.13224/j.cnki.jasp.2009.07.025
TU Baofeng, HU Jun, ZHAO Yong. Three-dimensional numerical research on stall inception in axial compressor[J]. Journal of Aerospace Power, 2009, 24(7): 1616-1621. (in Chinese) doi: 10.13224/j.cnki.jasp.2009.07.025
|
| [14] |
孙晓峰, 胡宗安, 冯毓诚, 等. 压气机旋转失速的一个气动声学模型[J]. 航空学报, 1991, 12(9): 467-473. SUN Xiaofeng, HU Zongan, FENG Yucheng, et al. An aeroacoustic model about the rotating stall of a compressor[J]. Acta Aeronautica et Astronautica Sinica, 1991, 12(9): 467-473. (in Chinese
SUN Xiaofeng, HU Zongan, FENG Yucheng, et al. An aeroacoustic model about the rotating stall of a compressor[J]. Acta Aeronautica et Astronautica Sinica, 1991, 12(9): 467-473. (in Chinese)
|
| [15] |
于巍巍, 王晓宇, 孙晓峰. 包含处理机匣影响的压气机旋转失速稳定性模型[J]. 航空动力学报, 2005, 20(5): 873-881. YU Weiwei, WANG Xiaoyu, SUN Xiaofeng. Investigation on the theoretical model combined with the novel casting treatmentwith rotating stall[J]. Journal of Aerospace Power, 2005, 20(5): 873-881. (in Chinese doi: 10.13224/j.cnki.jasp.2005.05.031
YU Weiwei, WANG Xiaoyu, SUN Xiaofeng. Investigation on the theoretical model combined with the novel casting treatmentwith rotating stall[J]. Journal of Aerospace Power, 2005, 20(5): 873-881. (in Chinese) doi: 10.13224/j.cnki.jasp.2005.05.031
|
| [16] |
于巍巍, 孙晓峰. 跨音压气机/风扇旋转失速稳定性模型[J]. 航空动力学报, 2005, 20(6): 1018-1027. YU Weiwei, SUN Xiaofeng. Rotating stall stability theory of the transonic axial compressors/fans[J]. Journal of Aerospace Power, 2005, 20(6): 1018-1027. (in Chinese doi: 10.13224/j.cnki.jasp.2005.06.021
YU Weiwei, SUN Xiaofeng. Rotating stall stability theory of the transonic axial compressors/fans[J]. Journal of Aerospace Power, 2005, 20(6): 1018-1027. (in Chinese) doi: 10.13224/j.cnki.jasp.2005.06.021
|
| [17] |
侯睿炜, 孙晓峰. 风扇/压气机数值稳定性模型[J]. 工程热物理学报, 2006, 27(1): 31-34. HOU Ruiwei, SUN Xiaofeng. A numerical stability model of rotating stall in axial fan/compressors[J]. Journal of Engineering Thermophysics, 2006, 27(1): 31-34. (in Chinese
HOU Ruiwei, SUN Xiaofeng. A numerical stability model of rotating stall in axial fan/compressors[J]. Journal of Engineering Thermophysics, 2006, 27(1): 31-34. (in Chinese)
|
| [18] |
刘小华, 周燕佩, 孙大坤, 等. 基于特征值理论的轴流跨声速压气机失稳预测[J]. 航空学报, 2014, 35(11): 2979-2991. LIU Xiaohua, ZHOU Yanpei, SUN Dakun, et al. Axial transonic compressor flow instability prediction based on eigenvalue theory[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(11): 2979-2991. (in Chinese
LIU Xiaohua, ZHOU Yanpei, SUN Dakun, et al. Axial transonic compressor flow instability prediction based on eigenvalue theory[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(11): 2979-2991. (in Chinese)
|
| [19] |
孙晓峰, 董旭, 张光宇, 等. 特征值理论在稳定性预测中的应用研究进展[J]. 航空学报, 2022, 43(10): 527408. SUN Xiaofeng, DONG Xu, ZHANG Guangyu, et al. Progress review of application of eigenvalue theory to stability prediction[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(10): 527408. (in Chinese
SUN Xiaofeng, DONG Xu, ZHANG Guangyu, et al. Progress review of application of eigenvalue theory to stability prediction[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(10): 527408. (in Chinese)
|
| [20] |
徐慎忍, 何晨, 孙大坤, 等. 基于高效特征值分析方法的旋转失速先兆预测[J]. 航空学报, 2023, 44(14): 628248. XU Shenren, HE Chen, SUN Dakun, et al. Efficient eigenvalue analysis method for rotating stall inception[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(14): 628248. (in Chinese
XU Shenren, HE Chen, SUN Dakun, et al. Efficient eigenvalue analysis method for rotating stall inception[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(14): 628248. (in Chinese)
|
| [21] |
DAY I J, CUMPSTY N A. The measurement and interpretation of flow within rotating stall cells in axial compressors[J]. Journal of Mechanical Engineering Science, 1978, 20(2): 101-114. doi: 10.1243/JMES_JOUR_1978_020_017_02
|
DownLoad:
