[1] |
BINDON J P.The measurement and formation of tip clearance loss[J].Journal of Turbomachinery,1989,111(3):257-263.
|
[2] |
DENTON J D.Loss mechanisms in turbomachines[J].Journal of Turbomachinery,1993,435(1):1-40.
|
[3] |
CHAN J K,YARAS M I,SJOLANDER S A.Interaction between inlet boundary layer,tip-leakage and secondary flows in a low-speed turbine cascade[R].Hague,Netherlands:International Gas Turbine and Aeroengine Congress and Exposition,American Society of Mechanical Engineers,1994.
|
[4] |
CAMCI C,DEY D,KAVURMACIOGLU L.Aerodynamics of tip leakage flows near partial squealer rims in an axial flow turbine stage[J].Journal of Turbomachinery,2005,127(1):14-24.
|
[5] |
HEYES F J,HODSON H P,DAILEY G M.The effect of blade tip geometry on the tip leakage flow in axial turbine cascades[J].Journal of Turbomachinery,1992,114(3):643-651.
|
[6] |
AMERI A,STEINTHORSSON E,RIGBY D.Effect of squealer tip on rotor heat transfer and efficiency[J].Journal of Turbomachinery,1998,120(4):753-759.
|
[7] |
高杰,郑群,刘云宁,等.涡轮叶片叶顶间隙变化减敏研究[J].航空动力学报,2015,30(11):2638-2646.GAO Jie,ZHENG Qun,LIU Yunning,et al.Investigation of desensitization of blade tip clearance variation in turbine blades[J].Journal of Aerospace Power,2015,30(11):2638-2646.(in Chinese)
|
[8] |
崔涛,陈绍文,周治华,等.深凹槽式涡轮叶顶间隙泄漏直列叶栅实验研究[J].工程热物理学报,2015,36(9):1902-1906.CUI Tao,CHEN Shaowen,ZHOU Zhihua,et al.Experimental research on deep double squealer tip clearance leakage flow in linear turbine cascade[J].Journal of Engineering Thermophysics,2015,36(9):1902-1906.(in Chinese)
|
[9] |
成锋娜,常海萍,张镜洋,等.突肩叶尖尾缘开槽对间隙流动换热特性的影响[J].航空动力学报,2016,31(2):383-390.CHENG Fengna,CHANG Haiping,ZHANG Jingyang,et al.Tip leakage flow and heat transfer characteristics with effect of trailing edge cutback on squealer tip[J].Journal of Aerospace Power,2016,31(2):383-390.(in Chinese)
|
[10] |
MOHAN K,GURUPRASAD S A.Effect of axially non-uniform rotor tip clearance on the performance of a high speed axial flow compressor stage[R].ASME Paper 94-GT-479,1994.
|
[11] |
WANG Z,JIA X,CAI R.Influence of blade tip clearance shapes on aerodynamic performance of an axial flow compressor stator[J].Journal of Power and Energy,2002,216(5)395-401.
|
[12] |
MA H,LI B.Effects of axial non-uniform tip clearances on aerodynamic performance of a transonic axial compressor[J].Journal of Thermal Science,2008,17(4):331-336.
|
[13] |
LU Hanan,LI Qiushi.Cantilevered stator hub leakage flow control and loss reduction using non-uniform clearances[J].Aerospace Science and Technology,2016,51:1-10.
|
[14] |
GAO J,ZHENG Q,LI Y,et al.Effect of axially non-uniform rotor tip clearance on aerodynamic performance of an unshrouded axial turbine[J].Journal of Power and Energy,2011,226(2):231-244.
|
[15] |
ZHOU Z,CHEN S,WANG S.Aerodynamic optimization of a winglet-cavity tip in a high-pressure axial turbine cascade[J].Journal of Aerospace Engineering,2018,232(4):649-663.
|
[16] |
LEE S,KWAK H.Tip leakage aerodynamics over stepped squealer tips in a turbine cascade[J].Experimental Thermal and Fluid Science,2011,35(1):135-145.
|
[17] |
LEE S W,KIM S U,KIM K H.Aerodynamic performance of winglets covering the tip gap inlet in a turbine cascade[J].International Journal of Heat and Fluid Flow,2012,34(1):36-46.
|
[18] |
LEE S W,CHEON J H,ZHANG Q.The effect of full coverage winglets on tip leakage aerodynamics over the plane tip in a turbine cascade[J].International Journal of Heat and Fluid Flow,2014,45(1):23-32.
|