[1] 夏联,崔健,顾扬.可调静叶对压气机低速性能影响的试验研究[J].燃气涡轮试验与研究,2005,18(1):31-34.XIA L,CUI J,GU Y.An experimental investigation on the effect of variable stator vane angle on compressor performance at low speed[J].Gas Tirbine Experiment and Reasearch,2005,18(1):31-34(in Chinese).
[2] VALKOV T V,TAN C S.Effect of upstream rotor vortical disturbances on the time-averaged performance of axial compressor stator.Part 2:Rotor tip vortex/streamwise vortex-stator blade interactions[J].Journal of Turbomachinery,1999,121(3):387-397.
[3] GBADEBO S A,CUMPSTY N A,HYNES T P.Three-dimensional separations in axial compressors[J].Journal of Turbomachinery,2005,127(2):331-339.
[4] MAILACH R,LEHMANN I,VOGELER K.Periodical unsteady flow within a rotor blade row of an axial compressor.Part 2:Wake-tip clearance vortex interaction[J].Journal of Turbomachinery,2008,130(4):041005.
[5] HAH C,BERGNER J,SCHIFFER H P.Tip clearance vortex oscillation,vortex shedding and rotating instabilities in an axial transonic compressor rotor[C]//ASME Turbo Expo 2008.New York:ASME,2008:57-65.
[6] KIELB R E,BARTWE J W,THOMAS J P,et al.Blade excitation by aerodynamic instabilities—A compressor blade study[C]//ASME Turbo Expo 2003.New York:ASME,2003:399-406.
[7] MAILACH R,VOGELER K.Unsteady aerodynamic blade excitation at the stability limit and during rotating stall in an axial compressor[C]//ASME Turbo Expo 2006.New York:ASME,2006:1701-1711.
[8] HOLZINGER F,WARTZEK F,JUNGST M,et al.Self-excited blade vibration experimentally investigated in transonic compressors:Rotating instabilities and flutter[J].Journal of Turbomachinery,2015,138(4):041006-1-041006-9.
[9] 张章.风扇/压气机气动弹性动力响应的机理与应用研究[D].北京:北京航空航天大学,2013.ZHANG Z.Investigation on the mechanism and application of aeroelastic dynamic respones in fan/compressor[D].Beijing:Beihang University,2013(in Chinese).
[10] 张明明.轴流压气机气动弹性失稳机理研究[D].北京:北京航空航天大学,2012.ZHANG M M.Investigation on the mechanism of aeroelasticity instability in axial compressor[D].Beijing:Beihang University,2012(in Chinese).
[11] YANG X D.Flow field and vibration behavior of the rotor due to mistuning IGV in a transonic compressor[C]//Proceeding of ASME 2012 International Mechanical Engineering Congress & Exposition.New York:ASME,2012:267-274.
[12] ZHANG M M,HOU A P,LI J X,et al.Analysis of blade vibration response induced by rotating stall in axial compressor[J].Journal of Aerospace Power,2012,27(10):2269-2277.
[13] 杜鹃.跨音压气机/风扇转子叶顶泄漏流动的非定常机制研究 [D].北京:中国科学院工程热物理研究所,2010.DU J.Investigation on the unsteady mechanism of tip leakage flow in transonic compressor/fan rotors[D].Beijing:Institute of Engineering Thermalphysics,Chinese Academy of Sciences,2010(in Chinese).
[14] BOHNE A,NIEHUIS R.Experimental off-design investigation of unsteady secondary flow phenomena in a three stage axial compressor at 68% nominal speed[C]//ASME Turbo Expo 2004.New York:ASME,2004:857-866.
[15] MAILACH R,LEHMANN I,VOGELER K.Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex[J].Journal of Turbomachinery,2000,123 (3):453-463.
[16] LEE S,RUNEHAL A K,KIM H J,et al.Large eddy simulation of unsteady flows in turbomachinery[J].Proceedings of the Institution of Mechanical Engineers,Part A:Journal of Power and Energy,2006,218(7):463-475. |