[1] |
DE LUCIA M, MENGONI C P, BONCINELLI P, et al. Synchronized LDV measurement in centrifugal impeller: seeding insemination set up and CFD comparison[C]//Proceedings of ASME Turbo Expo 2000: Power for Land, Sea, and Air. 2000. doi: 10.1115/2000-GT-0054
|
[2] |
WEICHERT S, DAY I. Detailed measurements of spike formation in an axial compressor[C]//Proceedings of ASME Turbo Expo 2012: Power for Land, Sea, and Air. 2012. doi: 10.1115/GT2012-68627
|
[3] |
YAMADA K,KIKUTA H,IWAKIRI K I,et al. An explanation for flow features of spike-type stall inception in an axial compressor rotor[J]. Journal of Turbomachinery,2013,135(2):021023. doi: 10.1115/1.4007570
|
[4] |
MA H W,WEI W. Experimental investigation of effects of distributed riblets on aerodynamic performance of a low-speed compressor[J]. Journal of Thermal Science,2013,22(6):592-599. doi: 10.1007/s11630-013-0667-1
|
[5] |
ZHENG X Q,LIU A X. Experimental investigation of surge and stall in a high-speed centrifugal compressor[J]. Journal of Propulsion and Power,2015,31(3):815-825. doi: 10.2514/1.B35448
|
[6] |
HE X,ZHENG X Q. Flow instability evolution in high pressure ratio centrifugal compressor with vaned diffuser[J]. Experimental Thermal and Fluid Science,2018,98:719-730. doi: 10.1016/j.expthermflusci.2018.06.023
|
[7] |
ZHENG X Q,SUN Z Z,KAWAKUBO T,et al. Experimental investigation of surge and stall in a turbocharger centrifugal com-pressor with a vaned diffuser[J]. Experimental Thermal and Fluid Science,2017,82:493-506. doi: 10.1016/j.expthermflusci.2016.11.036
|
[8] |
XUE X,WANG T. Stall recognition for centrifugal compressors during speed transients[J]. Applied Thermal Engineering,2019,153:104-112. doi: 10.1016/j.applthermaleng,2019.02.027
|
[9] |
XUE X,WANG T,ZHANG T T,et al. Mechanism of stall and surge in a centrifugal compressor with a variable vaned diffuser[J]. Chinese Journal of Aeronautics,2018,31(6):1222-1231. doi: 10.1016/j.cja.2018.04.003
|
[10] |
XUE X,WANG T. Experimental study on inducement and develop-ment of flow instabilities in a centrifugal compressor with different diffuser types[J]. Journal of Thermal Science,2020,29(2):435-444. doi: 10.1007/s11630-020-1223-4
|
[11] |
GREGORY J W,ASAI K,KAMEDA M,et al. A review of pressure-sensitive paint for high-speed and unsteady aerodynamics[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,2008,222(2):249-290. doi: 10.1243/09544100jaero243
|
[12] |
BENCIC T J. Rotating pressure and temperature measurements on scale-model fans using luminescent paints[C]//Proc of the 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. 1998. doi: 10.2514/6.1998-3452
|
[13] |
高丽敏,吴亚楠,胡小全,等. 基于光强的快速响应PSP动态测量技术及其应用[J]. 航空学报,2014,35(3):607-623. doi: 10.7527/S1000-6893.2013.0532GAO L M,WU Y N,HU X Q,et al. Intensity-based fast response PSP technique and its applications[J]. Acta Aeronautica et Astro-nautica Sinica,2014,35(3):607-623. doi: 10.7527/S1000-6893.2013.0532
|
[14] |
高丽敏,高杰,王欢,等. PSP技术在叶栅叶片表面压力测量中的应用[J]. 工程热物理学报,2011,32(3):411-414.GAO L M,GAO J,WANG H,et al. Application of PSP technique to pressure measurement on cascade surface[J]. Journal of Engineering Thermophysics,2011,32(3):411-414.
|
[15] |
曹传军,黄国平,梁德旺. 毫米级平面叶栅的PSP测量[J]. 实验流体力学,2010,24(1):68-73. doi: 10.3969/j.issn.1672-9897.2010.01.013CAO C J,HUANG G P,LIANG D W. The pressure measurement of millimeter level plane cascade using pressure sensitive paint[J]. Journal of Experiments in Fluid Mechanics,2010,24(1):68-73. doi: 10.3969/j.issn.1672-9897.2010.01.013
|
[16] |
PENG D,LIU Y Z. Fast pressure-sensitive paint for understanding complex flows: from regular to harsh environments[J]. Experiments in Fluids,2019,61(1):1-22. doi: 10.1007/s00348-019-2839-6
|
[17] |
CHESNAKAS C J,DANCEY C L. Three-component LDA measure-ments in an axial-flow compressor[J]. Journal of Propulsion and Power,1990,6(4):474-481. doi: 10.2514/3.25459
|
[18] |
HOBSON G V, DOBER D M. Three-dimensional fibre-optics LDV measurements in the endwall region of a linear cascade of controlled-diffusion stator blades[C]//Proceedings of ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition. 1994. doi: 10.1115/94-GT-352
|
[19] |
DOUKELIS A, MATHIOUDAKIS K, FOUNTI M, et al. 3D LDA measurements in an annular cascade for studying tip clearance effects[C]//Proceedings of the AGARD Conference. 1998.
|
[20] |
TANG G L. Measurements of the tip-gap turbulent flow structure in a low-speed compressor cascade[D]. Virginia: Virginia Tech, 2004.
|
[21] |
TIAN Q. Some features of tip gap flow fields of a linear compressor cascade[D]. Virginia: Virginia Tech, 2003.
|
[22] |
TIAN Q, SIMPSON R. Experimental study of tip leakage flow in the linear compressor cascade: part I - stationary wall[R]. AIAA-2007-269, 2007. doi: 10.2514/6.2007-269
|
[23] |
TIAN Q, SIMPSON R. Experimental study of tip leakage flow in the linear compressor cascade: part II - effect of moving wall[R]. AIAA-2007-270, 2007. doi: 10.2514/6.2007-270
|
[24] |
马宏伟,蒋浩康. 轴流压气机小流量状态转子叶尖泄漏涡三维紊流特性[J]. 航空动力学报,2000,15(4):347-352. doi: 10.3969/j.issn.1000-8055.2000.04.003MA H W,JIANG H K. 3-D turbulent characteristics of the tip leakage vortex inside an axial compressor rotor passage at a low mass-flow condition[J]. Journal of Aerospace Power,2000,15(4):347-352. doi: 10.3969/j.issn.1000-8055.2000.04.003
|
[25] |
马宏伟, 蒋浩康. 轴流压气机小流量状态转子泄漏涡的三维紊流特性[C]//中国工程热物理学会热机气动热力学学术会议. 1999.
|
[26] |
马宏伟,蒋浩康. 轴流压气机小流量状态转子叶尖泄漏涡的三维流动[J]. 工程热物理学报,2001,22(1):31-35. doi: 10.3321/j.issn:0253-231X.2001.01.010MA H W,JIANG H K. Three-dimensional flow of the tip leakage vortex inside an axial-flow compressor rotor passage at a low mass-flow condition[J]. Journal of Engineering Thermophysics,2001,22(1):31-35. doi: 10.3321/j.issn:0253-231X.2001.01.010
|
[27] |
马宏伟, 蒋浩康. 轴流压气机小流量状态转子泄漏涡的时均流动[C]//中国工程热物理学会热机气动热力学学术会议. 1999.
|
[28] |
于贤君. 亚音轴流压气机端壁区复杂流动研究及其模化分析[D]. 北京: 北京航空航天大学, 2009.
|
[29] |
YU X J,LIU B J,JIANG H K. Characteristics of the tip leakage vortex in a low-speed axial compressor[J]. AIAA Journal,2007,45(4):870-878. doi: 10.2514/1.25530
|
[30] |
MA H W,WEI W,WANG L X,et al. Experimental investigation of effects of suction-side squealer tip geometry on the flow field in a large-scale axial compressor using SPIV[J]. Journal of Thermal Science,2015,24(4):303-312. doi: 10.1007/s11630-015-0789-8
|
[31] |
LIU B J,WANG H W,LIU H X,et al. Experimental investigation of unsteady flow field in the tip region of an axial compressor rotor passage at near stall condition with stereoscopic particle image velocimetry[J]. Journal of Turbomachinery,2004,126(3):360-374. doi: 10.1115/1.1748367
|
[32] |
LIU B J, YU X J, WANG H W, et al. Evolution of the tip leakage vortex in an axial compressor rotor[C]//Proceedings of ASME Turbo Expo 2004: Power for Land, Sea, and Air. 2004. doi: 10.1115/GT2004-53703
|
[33] |
WANG L X, MA H W. Visualization study on the effects of the cascade parameters on the tip leakage flow in a compressor cascade[C]//Proc of the 14th Asian Symposium on Visualization. 2017.
|
[34] |
MA H W,WANG L X. Experimental study of effects of tip geometry on the flow field in a turbine cascade passage[J]. Journal of Thermal Science,2015,24(1):1-9. doi: 10.1007/s11630-015-0748-4
|
[35] |
杜朝辉,竺晓程. 激光测速技术及其在叶轮机械旋转流动中的应用[J]. 热力透平,2003,32(4):205-211. doi: 10.13707/j.cnki.31-1922/th.2003.04.001DU Z H,ZHU X C. Laser velocimeter and its application to rotating flow measurement in turbomachinery[J]. Thermal Turbine,2003,32(4):205-211. doi: 10.13707/j.cnki.31-1922/th.2003.04.001
|
[36] |
TROPEA C, YARIN A L, FOSS J F. Springer Handbook of Experimental Fluid Mechanics[M]. Springer Berlin Heidelberg, 2007.
|
[37] |
马宏伟,蒋浩康,聂超群. 轴流风机转子通道内尖区三维流场[J]. 工程热物理学报,1998,19(1):45-48.MA H W,JIANG H K,NIE C Q. Three-dimensional turbu-lent flow field in the tip region of an axial-flow fan rotor passage[J]. Journal of Engineering Thermophysics,1998,19(1):45-48.
|
[38] |
马宏伟,蒋浩康,徐月亭,等. 离心压气机转子内近端壁区三维紊流流场[J]. 航空动力学报,2000,15(4):342-346. doi: 10.13224/j.cnki.jasp.2000.04.002MA H W,JIANG H K,XU Y T,et al. Three-dimensional turbulent flow of the endwall region inside a centrifugal compressor impeller[J]. Journal of Aerospace Power,2000,15(4):342-346. doi: 10.13224/j.cnki.jasp.2000.04.002
|
[39] |
马宏伟,张庆国,蒋浩康. 轴流压气机转子叶尖泄漏涡和尾迹在静子尖区的传播[J]. 工程热物理学报,2002,23(4):437-440. doi: 10.3321/j.issn:0253-231X.2002.04.012MA H W,ZHANG Q G,JIANG H K. Transportation of rotor tip leakage vortex and rotor wake in an axial compressor stator passage[J]. Journal of Engineering Thermophysics,2002,23(4):437-440. doi: 10.3321/j.issn:0253-231X.2002.04.012
|
[40] |
ECKARDT D. Detailed flow investigations within a high-speed centrifugal compressor impeller[J]. Journal of Fluids Engineering,1976,98(3):390-399. doi: 10.1115/1.3448335
|
[41] |
ECKARDT D. Investigation of the jet-wake flow of a highly loaded centrifugal compressor impeller[R]. NASA-TM-75232, 1978.
|
[42] |
KRAIN H. A study on centrifugal impeller and diffuser flow[J]. Journal of Engineering for Power,1981,103(4):688-697. doi: 10.1115/1.3230791
|
[43] |
KRAIN H. Swirling impeller flow[J]. Journal of Turbomachinery,1988,110(1):122-128. doi: 10.1115/1.3262157
|
[44] |
ADLER D,LEVY Y. A laser-doppler investigation of the flow inside a backswept, closed, centrifugal impeller[J]. Journal of Mechanical Engineering Science,1979,21(1):1-6. doi: 10.1243/jmes_jour_1979_021_003_02
|
[45] |
HATHAWAY M D,CHRISS R M,WOOD J R,et al. Experimental and computational investigation of the NASA low-speed centrifugal compressor flow field[J]. Journal of Turbomachinery,1993,115(3):527-541. doi: 10.1115/1.2929285
|
[46] |
SKOCH G J, PRAHST P S, WERNET M P, et al. Laser anemometer measurements of the flow field in a 4: 1 pressure ratio centrifugal impeller[C]//Proceedings of ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. 1997. doi: 10.1115/97-GT-342
|
[47] |
SCHLEER M,ABHARI R S. Clearance effects on the evolution of the flow in the vaneless diffuser of a centrifugal compressor at part load condition[J]. Journal of Turbomachinery,2008,130(3):031009. doi: 10.1115/1.2776955
|
[48] |
METHEL J, GOODING W J, FABIAN J C, et al. The development of a low specific speed centrifugal compressor research facility[C]// Proceedings of ASME Turbo Expo 2016: Power for Land, Sea, and Air. 2016. doi: 10.1115/GT2016-56683
|
[49] |
GOODING W J,KEY N L. Leveraging LDV techniques for the investigation of unsteady turbomachinery flows[J]. The Aeronautical Journal,2019,123(1270):1919-1937. doi: 10.1017/aer.2019.28
|
[50] |
GOODING W J,FABIAN J C,KEY N L. Laser Doppler velocimetry characterization of unsteady vaned diffuser flow in a centrifugal compressor[J]. Journal of Turbomachinery,2020,142(4):041001. doi: 10.1115/1.4046230
|
[51] |
刘正先,曹淑珍,谷传纲,等. 离心叶轮内三维湍流流场的实验研究[J]. 工程热物理学报,1999,20(5):558-562.LIU Z X,CAO S Z,GU C G,et al. The experiment investigation of the flow field in centrifugal impeller[J]. Journal of Engineering Thermophysics,1999,20(5):558-562.
|
[52] |
刘正先,姜印平,曹淑珍,等. 离心叶轮内三维湍流流场的LDV测量[J]. 航空动力学报,2002,17(3):287-291. doi: 10.13224/j.cnki.jasp.2002.03.003LIU Z X,JIANG Y P,CAO S Z,et al. LDV measurements of three dimensional turbulent flow field in a centrifugal impeller[J]. Journal of Aerospace Power,2002,17(3):287-291. doi: 10.13224/j.cnki.jasp.2002.03.003
|
[53] |
刘正先,赵衡,曹淑珍,等. 不同工况对离心叶轮内部流场特性影响的实验研究[J]. 流体机械,2004,32(10):1-4. doi: 10.3969/j.issn.1005-0329.2004.10.001LIU Z X,ZHAO H,CAO S Z,et al. Experimental investigation of the character of flow field in centrifugal impeller at different flow rate[J]. Fluid Machinery,2004,32(10):1-4. doi: 10.3969/j.issn.1005-0329.2004.10.001
|
[54] |
PAONE N,RIETHMULLER M L,BRAEM-BUSSCHE R A. Experimental investigation of the flow in the vaneless diffuser of a centrifugal pump by particle image displacement velocimetry[J]. Experiments in Fluids,1989,7(6):371-378. doi: 10.1007/BF00193417
|
[55] |
POST M E, GOSS L P, BRAINARD L F. Two-color particle-imaging velocimetry in a turbine cascade[C]//Proc of the 29th Aerospace Sciences Meeting. 1991. doi: 10.2514/6.1991-274
|
[56] |
ESTEVADEORDAL J,GOGINENI S,COPENHAVER W,et al. Flow field in a low-speed axial fan: a DPIV investigation[J]. Experimental Thermal and Fluid Science,2000,23(1-2):11-21. doi: 10.1016/S0894-1777(00)00027-3
|
[57] |
WERNET M P. A flow field investigation in the diffuser of a high-speed centrifugal compressor using digital particle imaging velocimetry[J]. Measurement Science and Technology,2000,11(7):1007-1022. doi: 10.1088/0957-0233/11/7/316
|
[58] |
WERNET M P,BRIGHT M M,SKOCH G J. An investigation of surge in a high-speed centrifugal compressor using digital PIV[J]. Journal of Turbomachinery,2001,123(2):418-428. doi: 10.1115/1.1343465
|
[59] |
OHUCHIDA S,TAMAK H,KAWAKUBO T,et al. Internal flow measurements of turbomachinery using PIV[J]. IHI Engineering Review,2013,46(1):22-28.
|
[60] |
CUKUREL B,LAWLESS P B,FLEETER S. Particle image velocity investigation of a high speed centrifugal compressor diffuser: spanwise and loading variations[J]. Journal of Turbomachinery,2010,132(2):021010. doi: 10.1115/1.3104616
|
[61] |
HAYAMI H,HOJO M,ARAMAKI S. Flow measurement in a transonic centrifugal impeller Using a PIV[J]. Journal of Visualization,2002,5(3):255-261. doi: 10.1007/BF03182333
|
[62] |
VOGES M,BEVERSDORFF M,WILLERT C,et al. Application of particle image velocimetry to a transonic centrifugal compressor[J]. Experiments in Fluids,2007,43(2-3):371-384. doi: 10.1007/s00348-007-0279-1
|
[63] |
CUKUREL B, LAWLESS P, FLEETER S. PIV investigation of a high speed centrifugal compressor diffuser: circumferential and spanwise variations[R]. AIAA-2007-5021, 2007. doi: 10.2514/6.2007-5021
|
[64] |
UBBEN S,NIEHUIS R. Experimental investigation of the diffuser vane clearance effect in a centrifugal compressor stage with adjustable diffuser geometry—part I: compressor performance analysis[J]. Journal of Turbomachinery,2015,137(3):031003. doi: 10.1115/1.4028297
|
[65] |
UBBEN S,NIEHUIS R. Experimental investigation of the diffuser vane clearance effect in a centrifugal compressor stage with adjustable diffuser geometry: part II—detailed flow analysis[J]. Journal of Turbomachinery,2015,137(3):031004. doi: 10.1115/1.4028298
|
[66] |
GUILLOU E, GANCEDO M, DIMICCO R, et al. PIV measurements of surge incipience in a ported shroud compressor[R]. AIAA-2010-5110, 2010. doi: 10.2514/6.2010-5110
|
[67] |
GUILLOU E, GANCEDO M, DIMICCO R, et al. Surge investigation in a centrifugal compressor by stereoscopic PIV[R]. AIAA-2011-742, 2011. doi: 10.2514/6.2011-742
|
[68] |
GANCEDO M, GUTMARK E, GUILLOU E, et al. PIV measurements of flow in recirculation cavities at the inlet of a centrifugal compressor[R]. AIAA-2012-0454, 2012. doi: 10.2514/6.2012-454
|
[69] |
GUILLOU E,GANCEDO M,GUTMARK E,et al. PIV investigation of the flow induced by a passive surge control method in a radial compressor[J]. Experiments in Fluids,2012,53(3):619-635. doi: 10.1007/s00348-012-1310-8
|
[70] |
BANERJEE D,DEHNER R,SELAMET A,et al. Investigation of flow field at the inlet of a turbocharger com-pressor using digital particle image velocimetry[J]. Journal of Turbomachinery,2019,141(12):121003. doi: 10.1115/1.4044608
|