Citation: | WANG Zi-wei, LIU Dong-jian, CHEN Ti. Numerical Simulation of the Rotating Stall Feature on a Single Stage Transonic Compressor[J]. PHYSICS OF GASES, 2021, 6(1): 30-37. DOI: 10.19527/j.cnki.2096-1642.0787 |
[1] |
Day I, Morris S, et al. Spike-type compressor stall inception, detection, and control[J]. Annual Review of Fluid Mechanics, 2010, 42: 275-300. DOI: 10.1146/annurev-fluid-121108-145603
|
[2] |
钟勇健, 腾金芳, 徐玺, 等. 跨声速轴流压气机失速边界预测方法[J]. 航空动力学报, 2014, 29(8): 1838-1845. https://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201408012.htm
Zhong Y J, Teng J F, Xu X, et al. Prediction method of stall margin in axial-flow transonic compressor[J]. Journal of Aerospace Power, 2014, 29(8): 1838-1845(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201408012.htm
|
[3] |
屠宝锋. 风扇/压气机动态失速过程和多尺度非定常气动稳定性研究[D]. 南京: 南京航空航天大学, 2009.
Tu B F. Dynamic stall inception and multi-scale unsteady aerodynamic stability investigation of fan/compressor[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009(in Chinese).
|
[4] |
郭晋, 胡骏, 屠宝锋. 多级轴流压气机彻体力模型——理论方法及简化应用[J]. 航空动力学报, 2018, 33(8): 1954-1963. https://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201808019.htm
Guo J, Hu J, Tu B F. Body force model for multistage axial compressor-theoretical method and simplified application[J]. Journal of Aerospace Power, 2018, 33(8): 1954-1963(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201808019.htm
|
[5] |
禹世奇. 压气机近失速状态流场非定常特性研究[D]. 南京: 南京航空航天大学, 2012.
Yu S Q. Unsteady analysis of axial flow compressor at near stall conditions[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2012(in Chinese).
|
[6] |
鞠鹏飞, 宁方飞. 跨声压气机近失速流动特征的数值模拟研究[J]. 推进技术, 2016, 37(6): 1055-1064. https://www.cnki.com.cn/Article/CJFDTOTAL-TJJS201606008.htm
Ju P F, Ning F F. Numerical study of near-stall flow feature on transonic compressor[J]. Journal of Propulsion Technology, 2016, 37(6): 1055-1064(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-TJJS201606008.htm
|
[7] |
贺象, 银越千, 黄生勤, 等. 低速轴流压气机旋转失速演化机制研究[J]. 航空发动机, 2016, 42(5): 81-86. https://www.cnki.com.cn/Article/CJFDTOTAL-HKFJ201605015.htm
He X, Yin Y Q, Huang S Q, et al. Investigation on the rotating stall in a low-speed axial compressor[J]. Aeroengine, 2016, 42(5): 81-86(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKFJ201605015.htm
|
[8] |
李清鹏, 吴艳辉, 楚武利, 等. 轴流压气机转子近失速工况全通道数值模拟[J]. 航空动力学报, 2011, 26(10): 2330-2338. https://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201110023.htm
Li Q P, Wu Y H, Chu W L, et al. Full-annulus simulations on axial compressor rotor at near stall condition[J]. Journal of Aerospace Power, 2011, 26(10): 2330-2338(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201110023.htm
|
[9] |
吴艳辉, 王晓, 稂仿玉, 等. 单级轴流压气机失速起始的数值模拟[J]. 航空动力学报, 2014, 29(1): 125-132. https://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201401017.htm
Wu Y H, Wang X, Lang F Y, et al. Numerical simulation of stall inception in single-stage axial-flow compressor[J]. Journal of Aerospace Power, 2014, 29(1): 125-132(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201401017.htm
|
[10] |
Menon S, Schmidt D P. Conservative interpolation on unstructured polyhedral meshes: an extension of the supermesh approach to cell-centered finite-volume variables[J]. Computer Methods in Applied Mechanics and Engineering, 2011, 200(41/44): 2797-2804. http://www.sciencedirect.com/science/article/pii/S0045782511001666
|
[11] |
徐春光, 董海波, 刘君. 基于单元相交的混合网格精确守恒插值方法[J]. 爆炸与冲击, 2016, 36(3): 305-312. https://www.cnki.com.cn/Article/CJFDTOTAL-BZCJ201603003.htm
Xu C G, Dong H B, Liu J. An accurate conservative interpolation method for the mixed grid based on the intersection of grid cells[J]. Explosion and Shock Waves, 2016, 36(3): 305-312(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-BZCJ201603003.htm
|
[12] |
崔鹏程, 唐静, 李彬, 等. 基于超网格的重叠网格守恒插值方法[J]. 航空学报, 2018, 39(3): 121569. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201803003.htm
Cui P C, Tang J, Li B, et al. A conservative interpolation method for overset mesh via super mesh[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(3): 121569(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201803003.htm
|
[13] |
Reid L, Moore R D. 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 1.82[R]. NASA TP-1338, 1978.
|
[14] |
王子维, 范召林, 江雄, 等. 用于多级压气机非定常流动的谐波平衡方法研究[J]. 推进技术, 2017, 38(11): 2512-2521. https://www.cnki.com.cn/Article/CJFDTOTAL-TJJS201711014.htm
Wang Z W, Fan Z L, Jiang X, et al. Investigation on harmonic balance method for simulation of unsteady flow in the multi-stage compressor[J]. Journal of Propulsion Technology, 2017, 38(11): 2512-2521(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-TJJS201711014.htm
|
[15] |
Herrick G P, Hathaway M D, Chen J P. Unsteady full annulus simulations of a transonic axial compressor stage[R]. AIAA 2009-1059, 2009.
|
1. |
CAO Dongming,YUAN Caijia,WANG Dingxi,HUANG Xiuquan. Transition from Unsteady Flow Inception to Rotating Stall and Surge in a Transonic Compressor. Journal of Thermal Science. 2022(01): 120-129 .
![]() |