Improvement of Criterion for Prediction of Axial Compressor Corner Stall and Its Experimental Verification

被引：0
|
作者：
Liu B.-J. [1 ,2 ,3 ]
Qiu Y. [1 ]
Yu X.-J. [1 ,2 ,3 ]
An G.-F. [1 ,2 ,3 ]
机构：
[1] School of Energy and Power Engineering, Beihang University, Beijing
[2] National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University, Beijing
[3] Collaborative Innovation Center of Advanced Aero-Engine, Beijing
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2020年 / 41卷 / 03期
关键词：
Axial compressor; Corner separation; Corner stall; Criterion for the prediction of corner stall;
D O I：
10.13675/j.cnki.tjjs.190106
中图分类号：
学科分类号：
摘要：
Endwall corner separation is a typical secondary flow in axial compressor. With the increase of blade loading, the corner separation flow could develop into corner stall flow, which could cause serious flow blockage and loss in compressor blade passage and should be avoided during the compressor design procedure. In order to predict the corner stall flow in compressors, some criterions has been developed, which are mainly based on two-dimensional airfoil data. The endwall flow is strong three-dimensional in real compressor environment. A new criterion is developed accordingly in the present paper. The newly developed criterion was verified by experimental data obtained from low-speed compressor tests. The results showed that the existed criterions do not work well in real compressor environment and the newly developed criterion could accurately predict the stator hub corner stall in compressors with a critical value of D=0.405±0.02. In addition, the newly developed D parameter shows related correlation to the flow loss and blockage in compressor stators. © 2020, Editorial Department of Journal of Propulsion Technology. All right reserved.
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页码：527 / 536
页数：9
相关论文
共 20 条
  • [1] Cumpsty N.A., Compressor Aerodynamics, (1989)
  • [2] Gbadebo S.A., Cumpsty N.A., Hynes T.P., Three-Dimensional Separations in Axial Compressors, Journal of Turbomachinery, 127, 2, pp. 331-339, (2005)
  • [3] Lei V.M., Spakovszky Z.S., Greitzer E.M., A Criterion for Axial Compressor Hub-Corner Stall, Journal of Turbomachinery, 130, 3, (2008)
  • [4] Taylor J.V., Miller R.J., Competing Three-Dimensional Mechanisms in Compressor Flows, Journal of Turbomachinery, 138, 2, (2016)
  • [5] Joslyn H.D., Dring R.P., Axial Compressor Stator Aerodynamics, Journal of Engineering for Gas Turbines & Power, 106, 2, (1984)
  • [6] Schulz H.D., Gallus H.D., Experimental Investigation of the Three-Dimensional Flow in an Annular Compressor Cascade, Journal of Turbomachinery, 110, 4, pp. 467-478, (1988)
  • [7] Dong Y., Gallimore S.J., Hodson H.P., Three-Dimensional Flows and Loss Reduction in Axial Compressors, Journal of Turbomachinery, 109, 3, pp. 354-361, (1987)
  • [8] Gbadebo S.A., Cumpsty N.A., Hynes T.P., Interaction of Tip Clearance Flow and Three-Dimensional Separations in Axial Compressors, Journal of Turbomachinery, 128, 4, pp. 71-78, (2006)
  • [9] Breugelmans F.A.H., Carels Y., Demuth M., Influence of Dihedral on the Secondary Flow in a Two-Dimensional Compressor Cascade, Journal of Engineering for Gas Turbines & Power, 106, 3, pp. 578-584, (1984)
  • [10] Weingold H.D., Neubert R.J., Behlke R.F., Et al., Reduction of Compressor Stator Endwall Losses Through the Use of Bowed Stators
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