Thompson D W,King P I,Robe D C．Experimental investigation of stepped tip gap effects on the performance of a transonic axial-flow compressor rotor[J]．ASME Journal of Turbomachine,1998,120(3)：477-486．
[2]
曹朝辉,王如根,周敏,等．从压力面到吸力面开槽后叶栅特性的数值分析[J]．航空动力学报,2007,22(5)：814-817．Cao Chaohui, Wang Rugen, Zhou Min, et al．Numerical simulation on cascade characteristics with slot from pressure surface to suction surface[J]．Journal of Aerospace Power,2007,5：814-817(in Chinese)．
[3]
高杰,郑群．叶顶凹槽形态对动叶气动性能的影响[J]．航空学报,2013,34(2)：218-226．Gao Jie, Zheng Qun．Effect of squealer tip geometry on rotor blade aerodynamic performance[J]．Acta Aeronautica et Astronautica Sinica,2013,34(2)：218-226(in Chinese)．
[4]
岂兴明, 朴英, 周建兴, 等．涡轮叶顶间隙形态的优化[J]．吉林大学学报：工学版,2009,39(4)：873-879．Qi Xingming,Piao Ying,Zhou Jianxing,et al．Optimization design of turbine blade tip clearance shapes[J]．Journal of Jilin University：Engineering and Technology Edition,2009,39(4)：873-879(in Chinese)．
[5]
You D,Wang M,Moin P,et al．Prediction and analysis of rotor tip-clearance flows using large-eddy simulation [C]//IEEE Proceeding of the Users Group Conference,Williamsburg,VA,USA,2004．
[6]
Ameri A A,Steinthorsson E,Rigby D L．Effect of squealer tip on rotor heat transfer and efficiency [J]．Transactions-American Society of Mechanical Engineers Journal of Turbomachinery,1998,120(4)：753-759．
[7]
Saxena V,Nasir H,Ekkad S V．Effect of blade tip geometry on tip flow and heat transfer for a blade in a low-speed cascade[J]．Journal of Turbomachinery,2004,126(1)：130-138．
[8]
Nho Y C,Park J S,Lee Y J,et al．Effects of turbine blade tip shape on total pressure loss and secondary flow of a linear turbine cascade[J]．International Journal of Heat and Fluid Flow,2012,33(1)：92-100．
[9]
Mischo B,Behr T,Abhari R S．Flow physics and profiling of recessed blade tips：impact on performance and heat load[J]．Journal of Turbomachinery,2008,130(2)：1008-1015．
[10]
Prakash C,Lee C P,Cherry D G,et al．Analysis of some improved blade tip concepts[J]．Journal of Turbomachinery,2006,128(4)：639-642．
[11]
竺晓程．轴流通风机转子叶顶区流场的实验和数值研究[D]．上海：上海交通大学,2003．Zhu Xiaocheng．Experimental and numerical investigation of flow field in the tip region of an axial flow fan rator [D]．Shanghai：Shanghai Jiaotong University,2003(in Chinese)．
[12]
刘洋, 杨志刚．叶顶间隙对轴流风机内部流场影响的研究[J]．风机技术,2013(2)：9-14．Liu Yang,Yang Zhigang．Effect of blade tip clearance on the internal fluid field in axial-flow fan[J]．Fan Technology,2013(2)：9-14(in Chinese)．
[13]
李杨,欧阳华,杜朝辉．低压轴流风机周向弯曲叶片顶部间隙流动的数值分析[J]．动力工程,2006,26(5)：707-712．Li Yang,Ouyang Hua,Du Zhaohui．Numerical analysis of flow in tip clearances of circumferential bent blades of low pressure axial flow blowers[J]．Journal of Power Engineering,2006,26(5)：707-712(in Chinese)．
[14]
王军,姚瑞锋,刘静,等．低压轴流风机叶顶间隙对叶尖涡及外部性能的影响研究[J]．流体机械,2011,39(9)：26-29．Wang Jun,Yao Ruifeng,Liu Jing,et al．Influence of tip clearance on external performance and tip leakage vortex of low-pressure axial fan[J]．Fluid Machinery,2011,39(9)：26-29(in Chinese)．
[15]
李春曦,尹攀,叶学民．单动叶安装角深度异常对轴流风机性能及噪声影响的数值模拟[J]．中国电机工程学报,2012,32(35)：122-129．Li Chunxi,Yin Pan,Ye Xuemin．Simulation on performance and acoustic characteristics with deeply abnormal installation angle of single blade in a variable pitch axial fan[J]．Proceedings of the CSEE,2012,32(35)：122-129(in Chinese)．
[16]
李春曦,尹攀,叶学民,等．轴流风机动叶异常对风机内熵产影响的数值模拟[J]．动力工程学报,2012,32(12)：947-953．Li Chunxi,Yin Pan,Ye Xuemin,et al．Effect of abnormal blade incidence on internal entropy generation in axial-flow fans[J]．Journal of Chinese Society of Power Engineering,2012,32(12)：947-953(in Chinese)．
[17]
叶学民,李俊,李春曦,等．轴流风机多动叶安装角非同步调节下的内流特征和运行特性[J]．中国电机工程学报,2010,30(32)：77-83．Ye Xuemin,Li Jun,Li Chunxi,et al．Aerodynamics and operating performance of a variable pitch axial fan with asynchronous regulation of installation angles of multiple blades[J]．Proceedings of the CSEE,2010,30(32)：77-83(in Chinese)．
[18]
叶学民,李俊,王松岭,等．动叶可调轴流式通风机叶片安装角异常工况下的气动特性[J]．中国电机工学报,2009,29(26)：79-84．Ye Xuemin,Li Jun,Wang Songling,et al．Aerodynamics of adjustable blade axial fan under abnormal installation angles[J]．Proceedings of the CSEE,2009,29(26)：79-84(in Chinese)．
[19]
毛佳妮,曹紫胤．抑制叶顶间隙泄漏的叶轮机械叶片的流场模拟[J]．热能与动力工程,2009,24(2)：154-157．Mao Jiani,Cao Ziyin．Simulation of inhibition of tip clearance leakage flow fields of turbomachinery blades [J]．Journal of Engineering for Thermal Energy and Power,2009,24(2)：154-157(in Chinese)．
[20]
韩少冰,钟兢军,严红明．不同长度吸力面小翼对压气机叶栅间隙影响的数值研究[J]．航空动力学报,2011,26(3)：656-661．Han Shaobing,Zhong Jingjun,Yan Hongming．Influence of suction-side winglet length on tip leakage flow in compressor cascade[J]．Journal of Aerospace Power,2011,26(3)：656-661(in Chinese)．
[21]
昌泽舟．轴流式通风机实用技术[M]．北京：机械工业出版社,2005(3)：43-44．Chang Zezhou．Practical techniques of axial fan [M]．Beijing：China Machine Press,2005(3)：43-44(in Chinese)．
[22]
Venter S J．The effect of tip clearance on the performance of an axial flow fan[J]．Energy Conversion and Management,1992,33(2)：89-97．
[23]
Fukano T,Jang C M．Tip clearance noise of axial flow fans operating at design and off-design condition [J]．Journal of Sound and Vibration,2004,275(3/4/5)：1027-1050．
[24]
Inoue M,Kuroumaru M．Structure of tip clearance flow in an isolated axial compressor rotor[J]．Journal of Turbomachinery,1989,111(3)：250-256．
[25]
邓向阳．压气机叶顶间隙流的数值模拟[D]．北京：中国科学研究生院,2006．Deng Xiangyang．Numerical simulation of the compressor blade tip clearance flow[D]．Beijing：The Chinese Academy of Sciences,2006(in Chinese)．
