下端壁流向槽抽吸对高负荷扇形扩压叶栅性能影响的数值研究

推进技术 ›› 2018, Vol. 39 ›› Issue (8): 1753-1760.

下端壁流向槽抽吸对高负荷扇形扩压叶栅性能影响的数值研究

陆华伟¹,张海鑫¹,郭爽²,杨益¹,王旭¹

大连海事大学轮机工程学院，辽宁大连 116026,大连海事大学轮机工程学院，辽宁大连 116026,大连理工大学航空航天学院，辽宁大连 116024,大连海事大学轮机工程学院，辽宁大连 116026,大连海事大学轮机工程学院，辽宁大连 116026

发布日期:2021-08-15

Numerical Study on Effects of Streamwise GrooveSuction in Lower Endwall in a Highly-LoadedSectorial Compressor Cascade

Marine Engineering College，Dalian Maritime University，Dalian 116026，China,Marine Engineering College，Dalian Maritime University，Dalian 116026，China,School of Aeronautics and Astronautics，Dalian University of Technology，Dalian 116024，China,Marine Engineering College，Dalian Maritime University，Dalian 116026，China and Marine Engineering College，Dalian Maritime University，Dalian 116026，China

Published:2021-08-15

摘要/Abstract

摘要： 为探究附面层抽吸对亚声速高负荷扇形扩压叶栅气动性能和流场结构的影响，利用数值方法对叶栅进行了下端壁流向槽附面层抽吸的研究。对比原型和各抽吸方案发现:下端壁附面层的抽吸可以有效抑制下角区低能流体的分离及回流，降低下角区总压损失并提升叶栅近端壁区域的扩压能力，但上角区分离会略有加剧。当抽吸质量流量为原型叶栅质量流量的0.50%时，抽吸槽起始于角区分离点下游附近的抽吸方案(EW2)效果最佳，叶栅整体总压损失降低27.65%，静压比提升8.69%。

关键词: 端壁；流向槽抽吸；高负荷；扇形扩压叶栅；气动性能

Abstract: To explore the effects of boundary layer suction on aerodynamic performance and flow field structure in a subsonic highly-loaded sectorial compressor cascade， a research that streamwise groove boundary layer suction on the lower endwall， was completed by the method of numerical simulation. The improvement of different suction schemes was compared. The results show that the separation and back-flow in lower corner has been effectively restrained， the total pressure loss around the lower corner has been decreased and the diffusion capacity near lower endwall has been enhanced after the suction on lower endwall， but the separation in upper corner is slightly strengthened. The suction scheme with the groove starting slightly downstream the separation point of the corner region (EW2) is the best when the suction flow is 0.50% of the mass flow rate of the original cascade. The overall total pressure loss of cascade is reduced by 27.65%， and the static pressure ratio increased by 8.69%.

Key words: Endwall；Streamwise groove suction；Highly-loaded；Sectorial compressor cascade；Aerodynamic performance

陆华伟,张海鑫,郭爽,杨益,王旭. 下端壁流向槽抽吸对高负荷扇形扩压叶栅性能影响的数值研究[J]. 推进技术, 2018, 39(8): 1753-1760.

LU Hua-wei¹,ZHANG Hai-xin¹,GUO Shuang²,YANG Yi¹,WANG Xu¹. Numerical Study on Effects of Streamwise GrooveSuction in Lower Endwall in a Highly-LoadedSectorial Compressor Cascade[J]. Journal of Propulsion Technology, 2018, 39(8): 1753-1760.

参考文献

[1] Hosny W, Tabako W. An Analysis of Losses and Secondary Flow in Turbine Cascade[R]. AD 71-736853.
[2] 陆华伟, 阚晓旭, 钟兢军, 等. 正弯压气机静叶流道内流动结构分析[J]. 工程热物理学报, 2013, 34(10): 1828-1832.
[3] Bollapragada S. Presentation at Engineering Design Review[R]. AD 2000-A385216.
[4] Kerrebrock J L, Reijnen D P, Ziminsky W S. Aspirated Compressors[R]. ASME 97-GT-525.
[5] Schuler B J, Kerrebrock J L, Merchant A A, et al. Design, Analysis, Fabrication and Test of an Aspirated Fan Stage[R]. ASME 2000-GT-618.
[6] Merchant A A, Drela M, Kerrebrock J L. Aerodynamic Design and Analysis of a High Pressure Ratio Aspirated Compressor Stage[R]. ASME 2000-GT-619.
[7] Ali Merchant, Kerrebrock Jack L, Adamczyk John J. Experimental Investigation of a High Pressure Ratio Aspirated Fan Stage [R]. ASME 2004-GT-53679.
[8] Bolln G W Jr, Field K J, Burnes R. F414 Engine Today and Growth Potential for 21st Century Fighter Mission Challenges[R]. ISABE 99-7113.
[9] Liesner K, Meyer R. Experimental Setup for Detailed Secondary Flow Investigation by Two-Dimensional Measurement of Total Pressure Loss Coefficients in Compressor Cascades[C]. Belgium: VKI XIX Biannual Symposium on Measurement Techniques in Turbomachinery, 2008.
[10] Gmelin C, Thiele F, Liesner K, et al. Investigations of Secondary Flow Suction in a High Speed Compressor Cascade [R]. ASME 2011 GT-46479.
[11] Lemke M, Gmelin C, Thiele F. Simulations of a Compressor Cascade with Steady Secondary Flow Suction [J]. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 2013, 121(1): 549-556.
[12] 宋彦萍, 陈浮, 赵桂杰, 等. 附面层吸除对大转角压气机叶栅气动性能影响的数值模拟研究 [J]. 航空动力学报, 2005, 20(4): 561-566.
[13] 陈浮, 宋彦萍, 赵桂杰, 等. 附面层吸除对压气机叶栅稠度特性影响 [J]. 工程热物理学报, 2005, 26(2): 211-215.
[14] 张华良, 谭春青, 张新敬, 等. 采用附面层抽吸(BLS)控制流动分离的数值模拟 [J]. 推进技术, 2009, 30(2): 192-196. (ZHANG Hua-liang, TAN Chun-qing, ZHANG Xin-jing, et al. Numerical Investigation on Application of Boundary Layer Suction to Control the Flow Separations[J]. Journal of Propulsion Technology, 2009, 30(2): 192-196.)
[15] 郭爽, 陈浮, 陆华伟, 等. 端壁抽吸位置对大转角扩压叶栅流场及负荷的影响 [J]. 推进技术, 2011, 32(3): 323-328. (GUO Shuang, CHEN Fu, LU Hua-wei, et al. Effects of Endwall Boundary Layer Suction Position on the Flow Field and Load in a High-Turning Compressor Cascade[J]. Journal of Propulsion Technology, 2011, 32(3): 323-328.)
[16] 郭爽, 陆华伟, 宋彦萍, 等. 端壁附面层抽吸对大转角扩压叶栅旋涡影响的实验研究[J]. 推进技术, 2013, 34(11): 1466-1473. (GUO Shuang, LU Hua-wei, SONG Yan-ping, et al. Experimental Investigation on Effects of Endwall Boundary Layer Suction on Vortexes of High-Turning Compressor Cascades[J]. Journal of Propulsion Technology, 2013, 34(11): 1466-1473.)
[17] 阚晓旭. 矩形扩压叶栅中应用叶尖小翼的性能研究 [D]. 大连:大连海事大学, 2012.