Coupling Method and Mechanism of Stability Enhancement for Endwall Stall in Axial Flow Compressor
1.Faculty of Water Resources and Hydroelectric Engineering,Xi’an University of Technology,Xi’an710048,China;2.State Key Laboratory of Eco-Hydraulic in Northwest Arid Region,Xi’an University of Technology,Xi’an710048,China;3.School of Power and Energy,Northwestern Polytechnical University,Xi’an710072,China;4.Collaborative Innovation Center of Advanced Aero-Engine,Beijing100191,China
WANG Wei1,2,ZHANG Xiang1,LU Jin-ling1,2,LUO Xing-qi1,2,CHU Wu-li3,4. Coupling Method and Mechanism of Stability Enhancement for Endwall Stall in Axial Flow Compressor[J]. Journal of Propulsion Technology, 2020, 41(3): 544-552.
[1] Fujita H,Takata H.A Study on Configurations of Casing Treatment for Axial Flow Compressors[J].Bulletin of the JSME,1987,27(1):1675-1681.
[2] Hathaway M D.Passive Endwall Treatments for Enhancing Stability[R].NASA/TM-2007-214409.
[3] 张燕东,陆亚钧.圆弧斜槽处理机匣的实验研究[J].航空动力学报,1998,13 (3):254-258.
[4] Ross M H,Cameron J D,Morris S C,et al.Axial Compressor Stall, Circumferential Groove Casing Treatment, and the Tip-Clearance Momentum Flux [J]Journal of Propulsion and Power,2017,34(1):146-152.
[5] Du Juan,Li Fan,Li Jichao,et al.A Study of Performance and Flow Mechanism of a Slot-Groove Hybrid Casing Treatment in a Low-Speed Compresso[R].ASME 2015-GT-43920.
[6] Ma Ning,Nan Xi,Lin Feng.Numerical Study on Effects of Axial-Slot Casing Treatment on Peak Efficiency of Axial Compressors[R].ASME 2016-GT-56554
[7] Suder K L,Hathaway M D,Thorp S A,et al.Compressor Stability Enhancement Using Discrete Tip Injection[R].ASME2000-GT-0650.
[8] Strazisar A J,Bright M M,Thorp S,et al.Compressor Stall Control Through Endwall Recirculation[R].ASME 2004-GT-54295.
[9] Sun Dakun,Sun Xiaofeng,Liu Xiaohua,et al.Effect of Novel Casing Treatment on the Suppression of Stall Precursor in a Transonic Compressor[R].ASME 2014-GT-26439.
[10] 吴 云,李应红.等离子体流动控制研究进展与展望[J].航空学报,2015,36(2):381-405.
[11] Ali Arshad ,Li Qiushi,Li Simin,et al.Effects of Inlet Radial Distortion on the Type of Stall Precursor in Low-Speed Axial Compressor[J].Journal of Aerospace Engineering,2018,232(1):55-67.
[12] Matthias R,Martin L,Konrad V,et al.Experimental and Numerical Investigation of a Circumferential Groove Casing Treatment in a Low Speed Axial Research Compressor at Different Tip Clearances[R].ASME2017-GT-6305.
[13] 王永明,胡 骏,屠宝锋,等.带处理机匣的跨声速风扇非定常数值模拟[J].南京航空航天大学学报,2006,38(5):540-544.
[14] Cumpsty N A.Compressor Aerodynamics[M].Melbourne:Krieger Pub. Co.,2004.
[15] Wilke I,Kau H P,Brignole G.Numerically Aided Design of a High-Efficient Casing Treatment for a Transonic Compressor[R].ASME 2005-GT-68993.
[16] Greitzer E M,Nikkanen J P,Haddad D E,et al.A Fundamental Criterion for the Application of Rotor Casing Treatment[J].Journal of Fluids Engineering,1979,101(2):237-243.
[17] Cheng P,Prell M E ,Greitzer E M,et al.Effects of Compressor Hub Treatment on Stator Stall and Pressure Rise[J].AIAA Journal of Aircraft,1984,21 (7):469-475.
[18] Heinichen F,Gummer V,Schiffer H P.Numerical Investigation of a Single Circumferential Groove Casing Treatment on Three Different Compressor Rotors[R].ASME 2011-GT-45905.
[19] 王 维,楚武利,张皓光.高负荷两级轴流压气机耦合型机匣处理的设计研究[J].推进技术,2017,38 (10):2365-2373.(WANG Wei, CHU Wu-li, ZHANG Hao-guang.Study of Design of a Coupled Casing Treatment for a Two-Stage High-Loaded Axial Flow Compressor[J].Journal of Propulsion Technology,2017,38 (10):2365-2373.)
[20] 卢新根.轴流压气机内部流动失稳及其被动控制策略研究[D].西安:西北工业大学,2007.
[21] Wang Wei,Chu Wuli,Zhang Haoguang,et al.Experimental Study of Self-Recirculating Casing Treatment in a Subsonic Axial Compressor[J].Journal of Power and Energy,2016,230 (8):805-818.
[22] Wang Wei,Chu Wuli,Zhang Haoguang,et al.Experimental and Numerical Study of Tip Injection in a Subsonic Axial Flow Compressor [J].Chinese Journal of Aeronautics,2017,30 (3):907-917.
[23] Wang Wei,Chu Wuli,Zhang Haoguang.Numerical Investigation on the Effect of a Plenum Chamber with Slot-type Casing Treatment on the Performance of an Axial Transonic Compressor[J].Journal of Power and Energy,2015,229 (4):393-405.