| Citation: | MAO Xiaochen, DING Zhihua, WANG Yunyu, et al. Effect of endwall movement on aerodynamic performance and tip flow characteristics of tandem diffusion cascades[J]. Journal of Aerospace Power, 2025, 40(12):20240737 doi: 10.13224/j.cnki.jasp.20240737 |
Numerical simulation methods were employed to quantitatively and qualitatively explore the impact of endwall movement on the aerodynamic performance and tip flow characteristics of tandem diffusion cascades from the perspectives of entropy production rate, blockage factor and kinetic energy component of leakage flow. The main conclusions were as follows: firstly, after the endwall movement, the overall loss of tandem cascade was reduced, the blockage in tip area was intensified, and the flow turning angle was decreased, while the lag angle was increased. In the range of −4° to 4° angle of incidence, the loss was reduced by more than 3.9%, and the blockage was increased by more than 30.4%. Secondly, the endwall movement increased the leakage flow of the front and rear blades by 12.3% and 9.9%, respectively, but decreased the gap jet flow. Furthermore, the endwall movement enlarged the ratio of the kinetic energy of the leakage flows of the front and rear blades, with the secondary flow kinetic energy becoming dominant. It also increased the loads on the front and rear blades and made the position of the maximum pressure difference move forward in advance. As a result, the morphology and development of the leakage vortices were changed and the formation of the jet vortices was suppressed. In addition, the endwall movement significantly weakened the endwall shear effect and the mixing effect of the gap jet, expanded the circumferential influence range of the leakage flow of the front blade and caused secondary leakage. This resulted in a significant reduction in the entropy production of the front blade, while the change in the entropy production of the rear blade was relatively small. Moreover, the blockages of both the front and rear blades were intensified. The impact of the endwall movement and the increase in the angle of incidence on the front blade of the tandem cascades was greater than that on the rear blade, which was mainly the result of the regulating effect of the gap jet.
| [1] |
DENTON J D. Loss mechanisms in turbomachines[J]. Journal of Turbomachinery, 1993, 115(4): 621-656. doi: 10.1115/1.2929299
|
| [2] |
MAYNARD J M, WHEELER A P S, TAYLOR J V, et al. Unsteady structure of compressor tip leakage flows[J]. Journal of Turbomachinery, 2023, 145(5): 051005. doi: 10.1115/1.4055769
|
| [3] |
KANG S, HIRSCH C. Numerical simulation of three-dimensional viscous flow in a linear compressor cascade with tip clearance[J]. Journal of Turbomachinery, 1996, 118(3): 492-502. doi: 10.1115/1.2836694
|
| [4] |
韩少冰, 钟兢军, 严红明. 端壁相对运动对压气机叶栅间隙流场影响的数值模拟[J]. 动力工程学报, 2011, 31(4): 257-262. HAN Shaobing, ZHONG Jingjun, YAN Hongming. Influence of endwall relative movement on tip clearance flow in a compressor cascade[J]. Journal of Chinese Society of Power Engineering, 2011, 31(4): 257-262. (in Chinese
HAN Shaobing, ZHONG Jingjun, YAN Hongming. Influence of endwall relative movement on tip clearance flow in a compressor cascade[J]. Journal of Chinese Society of Power Engineering, 2011, 31(4): 257-262. (in Chinese)
|
| [5] |
侯杰萱, 柳阳威, 陆利蓬. 移动端壁对压气机叶栅中叶尖泄漏流动的影响[J]. 航空动力学报, 2018, 33(4): 803-811. HOU Jiexuan, LIU Yangwei, LU Lipeng. Effects of moving endwall on tip leakage flow in compressor cascade[J]. Journal of Aerospace Power, 2018, 33(4): 803-811. (in Chinese
HOU Jiexuan, LIU Yangwei, LU Lipeng. Effects of moving endwall on tip leakage flow in compressor cascade[J]. Journal of Aerospace Power, 2018, 33(4): 803-811. (in Chinese)
|
| [6] |
吴艳辉, 楚武利, 刘志伟. 移动壁对压气机叶栅间隙流动的影响[J]. 航空动力学报, 2006, 21(1): 112-118. WU Yanhui, CHU Wuli, LIU Zhiwei. Influence of moving end-wall on tip clearance flow in an axial-flow compressor cascade[J]. Journal of Aerospace Power, 2006, 21(1): 112-118. (in Chinese doi: 10.3969/j.issn.1000-8055.2006.01.021
WU Yanhui, CHU Wuli, LIU Zhiwei. Influence of moving end-wall on tip clearance flow in an axial-flow compressor cascade[J]. Journal of Aerospace Power, 2006, 21(1): 112-118. (in Chinese) doi: 10.3969/j.issn.1000-8055.2006.01.021
|
| [7] |
YANG Chengwu, LU Xingen, ZHANG Yanfeng, et al. Numerical investigation of a cantilevered compressor stator at varying clearance sizes: ASME Paper GT2015-42124[R]. Montreal, Canada: ASME, 2015.
|
| [8] |
JIANG Chao, HU Jun, WANG Jiayu, et al. The effect of tip clearance and hub rotation on the performance of an axial compressor stator: ASME Paper GTINDIA2019-2622[R]. Chennai, India: ASME, 2019.
|
| [9] |
HOU Jiexuan, LIU Yangwei. Effect of moving end wall on tip leakage flow in a compressor cascade with different clearance heights[J]. AIP Advances, 2024, 14(1): 015327. doi: 10.1063/5.0184929
|
| [10] |
VENTOSA-MOLINA J, LANGE M, MAILACH R, et al. Study of relative endwall motion effects in a compressor cascade through direct numerical simulations[J]. Journal of Turbomachinery, 2021, 143(1): 011005. doi: 10.1115/1.4049101
|
| [11] |
安广丰, 范竹, 于贤君, 等. 端壁移动对悬臂静子气动性能的影响[J]. 航空动力学报, 2024, 39(4): 20210564. AN Guangfeng, FAN Zhu, YU Xianjun, et al. Effects of endwall movement on the aerodynamic performance of cantilevered stators[J]. Journal of Aerospace Power, 2024, 39(4): 20210564. (in Chinese
AN Guangfeng, FAN Zhu, YU Xianjun, et al. Effects of endwall movement on the aerodynamic performance of cantilevered stators[J]. Journal of Aerospace Power, 2024, 39(4): 20210564. (in Chinese)
|
| [12] |
QIANG Xiaoqing, DENG Hefang, XIA Kailong, et al. Effects of moving endwall on the unsteadiness of tip leakage flow in compressor cascades[J]. Physics of Fluids, 2023, 35(8): 085116. doi: 10.1063/5.0159912
|
| [13] |
DENG Hefang, XIA Kailong, TENG Jinfang, et al. Analysis of leakage flow and loss in a linear compressor cascade with moving endwall[J]. Aerospace Systems, 2023, 6(1): 107-118. doi: 10.1007/s42401-022-00173-7
|
| [14] |
LIU Baojie, ZHANG Chuanhai, AN Guangfeng, et al. Using tandem blades to break loading limit of highly loaded axial compressors[J]. Chinese Journal of Aeronautics, 2022, 35(4): 165-175. doi: 10.1016/j.cja.2021.07.031
|
| [15] |
BAMMERT K, STAUDE R. Optimization for rotor blades of tandem design for axial flow compressors[J]. Journal of Engineering for Power, 1980, 102(2): 369-375. doi: 10.1115/1.3230263
|
| [16] |
BAMMERT K, BEELTE H. Investigations of an axial flow compressor with tandem cascades[J]. Journal of Engineering for Power, 1980, 102(4): 971-977. doi: 10.1115/1.3230369
|
| [17] |
SACHMANN J, FOTTNER L. Highly loaded tandem compressor cascade with variable camber and stagger: ASME Paper 93-GT-235[R]. Cincinnati, US: ASME, 1993.
|
| [18] |
MOHSEN M, OWIS F M, HASHIM A A. The impact of tandem rotor blades on the performance of transonic axial compressors[J]. Aerospace Science and Technology, 2017, 67: 237-248. doi: 10.1016/j.ast.2017.04.019
|
| [19] |
KUMAR A, PRADEEP A M. Design and off-design behavior of a tandem rotor stage[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020, 234(4): 927-942. doi: 10.1177/0954410019893162
|
| [20] |
BABU S, CHATTERJEE P, PRADEEP A M. Transient nature of secondary vortices in an axial compressor stage with a tandem rotor[J]. Physics of Fluids, 2022, 34(6): 065125. doi: 10.1063/5.0092226
|
| [21] |
PAYYAPPALLI M M, PRADEEP A M. Effect of tandem blading in contra-rotating axial flow fans: ASME Paper GT2018-75477[R]. Oslo, Norway: ASME, 2018.
|
| [22] |
HAN Le, YUAN Wei, WANG Yanrong. Influence of tip leakage flow and ejection on stall mechanism in a transonic tandem rotor[J]. Aerospace Science and Technology, 2018, 77: 499-509. doi: 10.1016/j.ast.2018.04.007
|
| [23] |
SINGH A, MISTRY C S. Study on effect of axial overlap on tip leakage flow structure in tandem bladed low speed axial flow compressor: ASME Paper GT2019-91366[R]. Phoenix, US: ASME, 2019.
|
| [24] |
CAO Zhiyuan, GAO Xi, SONG Cheng, et al. Performance enhancing for a highly loaded tandem cascade by endwall incoming vortex-corner separation interaction[J]. Proceedings of the Institution of Mechanical Engineers: Part C Journal of Mechanical Engineering Science, 2021, 235(23): 6833-6846. doi: 10.1177/09544062211018713
|
| [25] |
SCHNEIDER T, KOŽULOVIĆ D. Flow characteristics of axial compressor tandem cascades at large off-design incidence angles: ASME Paper GT2013-94708[R]. San Antonio, US: ASME, 2013.
|
| [26] |
MANAS M P, SHINE S R. Characterization of tandem airfoil configurations of axial compressors[J]. International Journal of Turbo and Jet-Engines, 2022, 39(2): 167-181.
|
| [27] |
KUMAR A, CHHUGANI H, MORE S, et al. Effect of differential tip clearance on the performance of a tandem rotor: ASME Paper GT2021-59007 [R]. Virtual, Online: ASME, 2021.
|
| [28] |
MAO Xiaochen, LIU Bo, ZHANG Botao. Hub clearance effects of a cantilevered tandem stator on the performance and flow behaviors in a small-scale axial flow compressor[J]. Aerospace Science and Technology, 2019, 91: 219-230. doi: 10.1016/j.ast.2019.05.011
|
| [29] |
KONRATH L, PEITSCH D, HEINRICH A. An analysis of the secondary flow around a tandem blade under the presence of a tip gap in a high-speed linear compressor cascade[J]. Journal of Turbomachinery, 2022, 144(10): 101003. doi: 10.1115/1.4051558
|
| [30] |
LIESNER K, MEYER R. Combination of active and passive flow control in a high speed compressor cascade: ASME Paper GT2014-25662[R]. Düsseldorf, Germany: ASME, 2014.
|
| [31] |
YANG Zonghao, LIU Bo, MAO Xiaochen, et al. Numerical investigation of inlet boundary layer in an axial compressor tandem cascade[J]. Energies, 2022, 15(18): 6850. doi: 10.3390/en15186850
|
| [32] |
ECKEL J, HEINRICH A, JANKE C, et al. 3D numerical and experimental investigation of high turning compressor tandem cascades[C]//Proceedings of Deutscher Luft-Und Raumfahrtkongress. Braunschweig, Germany: [s. n. ], 2016: 1-13.
|
| [33] |
ZHANG Botao, MAO Xiaochen, LIU Bo, et al. Complicated flow in tip flow field of a compressor tandem cascade using delayed detached eddy simulation[J]. Chinese Journal of Aeronautics, 2024, 37(8): 63-78. doi: 10.1016/j.cja.2024.03.044
|
| [34] |
MEYER R, BECHERT D, HAGE W. Secondary flow control oncompressor blades to improve the performance of axial turbomachines[R]. Prague, The Czech Republic: [s. n. ], 2003.
|
| [35] |
LIESNER K, MEYER R, LEMKE M, et al. On the efficiency of secondary flow suction in a compressor cascade: ASME Paper GT2010-22336[R]. Glasgow, UK: ASME, 2010.
|
| [36] |
HERGT A, MEYER R, LIESNER K, et al. A new approach for compressor endwall contouring: ASME Paper GT2011-45858[R]. Vancouver, Canada: ASME, 2011.
|
| [37] |
CHEN Pingping, QIAO Weiyang, LIESNER K, et al. Location effect of boundary layer suction on compressor hub-corner separation: ASME Paper GT2014-25043[R]. Düsseldorf, Germany: ASME, 2014.
|
| [38] |
LIU Jianming, LIU Chaoqun. Modified normalized Rortex/vortex identification method[J]. Physics of Fluids, 2019, 31(6): 061704. doi: 10.1063/1.5109437
|
| [39] |
HUNT J C R, WRAY A A, MOIN P. Eddies, stream, and convergence zones in turbulent flows[R]. Washington, DC: NASA, 1988.
|
| [40] |
CHAKRABORTY P, BALACHANDAR S, ADRIAN R J. On the relationships between local vortex identification schemes[J]. Journal of Fluid Mechanics, 2005, 535: 189-214. doi: 10.1017/S0022112005004726
|
| [41] |
LIU Chaoqun, GAO Yisheng, DONG Xiangrui, et al. Third generation of vortex identification methods: Omega and Liutex/Rortex based systems[J]. Journal of Hydrodynamics, 2019, 31(2): 205-223. doi: 10.1007/s42241-019-0022-4
|
| [42] |
LIU Chaoqun, WANG Yiqian, YANG Yong, et al. New omega vortex identification method[J]. Science China Physics, Mechanics & Astronomy, 2016, 59(8): 684711.
|
| [43] |
DONG Xiangrui, WANG Yiqian, CHEN Xiaoping, et al. Determination of epsilon for Omega vortex identification method[J]. Journal of Hydrodynamics, 2018, 30(4): 541-548. doi: 10.1007/s42241-018-0066-x
|
| [44] |
ZHANG Yuning, QIU Xu, CHEN Feipeng, et al. A selected review of vortex identification methods with applications[J]. Journal of Hydrodynamics, 2018, 30(5): 767-779. doi: 10.1007/s42241-018-0112-8
|
| [45] |
BRENNAN G, HARVEY N W, ROSE M G, et al. Improving the efficiency of the Trent 500-HP turbine using nonaxisymmetric end walls: Part Ⅰ turbine design[J]. Journal of Turbomachinery, 2003, 125(3): 497-504. doi: 10.1115/1.1450766
|
| [46] |
REISING S, SCHIFFER H P. Non-axisymmetric end wall profiling in transonic compressors: Part Ⅱ design study of a transonic compressor rotor using non-axisymmetric end walls: optimization strategies and performance: ASME Paper GT2009-59134[R]. Orlando, US: ASME, 2009.
|
| [47] |
YOON S, SELMEIER R, CARGILL P, et al. Effect of the stator hub configuration and stage design parameters on aerodynamic loss in axial compressors[J]. Journal of Turbomachinery, 2015, 137(9): 091001. doi: 10.1115/1.4029598
|
| [48] |
WANG Wei, WANG Jun, LIU Hui, et al. CFD prediction of airfoil drag in viscous flow using the entropy generation method[J]. Mathematical Problems in Engineering, 2018, 2018: 4347650.
|
| [49] |
ZHANG Luying, KRITIOTI L, WANG Peng, et al. A detailed loss analysis methodology for centrifugal compressors: ASME paper GT2021-59334[R]. Virtual, Online: ASME, 2021.
|
| [50] |
LIU Baojie, AN Guangfeng, YU Xianjun, et al. Experimental investigation of the effect of rotor tip gaps on 3D separating flows inside the stator of a highly loaded compressor stage[J]. Experimental Thermal and Fluid Science, 2016, 75: 96-107. doi: 10.1016/j.expthermflusci.2016.02.006
|
| [51] |
HOU Jiexuan, LIU Yangwei. Evolution of unsteady vortex structures in the tip region of an axial compressor rotor[J]. Physics of Fluids, 2023, 35(4): 045107. doi: 10.1063/5.0141818
|
| [52] |
TALLMAN J, LAKSHMINARAYANA B. Numerical simulation of tip leakage flows in axial flow turbines, with emphasis on flow physics: Part Ⅱ effect of outer casing relative motion[J]. Journal of Turbomachinery, 2001, 123(2): 324-333. doi: 10.1115/1.1369113
|
| [53] |
MAO Xiaochen, WANG Yunyu, DING Zhihua, et al. Design strategy and relevant flow mechanisms of highly loaded 3D compressor tandem cascades[J]. Chinese Journal of Aeronautics, 2024, 37(7): 220-235. doi: 10.1016/j.cja.2024.04.025
|