Hah C．Aerodynamic lean and sweep for improvements in compressor performances,Lecture Series 1999-02[R]．Flanders,Belgium：Von Karman Institute for Fluid Dynamics,Turbomachinery Blade Design Systems, 1999．
[2]
Wang Z Q．Three-Dimensional theory and design method of bowed-twisted blade and its application,Lecture Series 1999-02[R]．Flanders,Belgium：Von Karman Institute for Fluid Dynamics,Turbomachinery Blade Design Systems, 1999．
[3]
Breugelmans F A E．Influence of incidence angle on the secondary flow in compressor cascade with different dihedral distribution[C]//International Symposium on Air Breathing Engines,7th,Beijing,1985．
[4]
Breugelmans F A E,Carels Y,Demuth M．Influence of dihedral on the secondary flow in a two dimensional compressor cascade[J]．Journal of Engineering for Gas Turbine and Power,1984(106)：578-584．
[5]
Gallimore S J,Bolger J J,Cumpsty A,et al．The use of sweep and dihedral in multistage axial flow compressor blading,Part 1：university research and methods development[C]//American Society of Mechanical Engineers Turbomachinery Exposition,Amsterdam,The Netherlands,GT-2002-30328,2002．
[6]
Gallimore S J,Bolger J J,Cumpsty N A,et al．The Use of Sweep and Dihedral in Multistage Axial Flow Compressor Blading,Part 2：Low and High Speed Designs and Test Verification[C]//American Society of Mechanical Engineers Turbomachinery Exposition,Amsterdam,The Netherlands,GT-2002-30329,2002．
[7]
Sasaki T,Breugelmans F A E．Comparison of sweep and dihedral effects on compressor cascade performance[J]．Journal of Turbomachinery,1998,120(2)：454-464．
[8]
Fischer A,Riess W,Seume J R．Performance of strongly bowed stators in a 4-stage high speed compressor[C]//American Society of Mechanical Engineers Turbomachinery Exposition,Atlanta,USA,GT2003-38392,2003．
[9]
钟兢军,王苇,苏杰先,等．稠度对弯曲叶片压气机叶栅特性的影响[J]．航空动力学报,1997,12(2)：163-166． Zhong Jingjun,Wang Wei,Su Jiexian,et al．Effects of solidity on characteristics of compressor cascade with curved-blade[J]．Journal of Aerospace Power,1997,12(2)：163-166(in Chinese)．
[10]
苏杰先,王仲奇．叶片的弯扭联合气动成型理论、实验、设计及其应用[J]．动力工程,1992,12(6)：1-6． Su Jiexian,Wang Zhongqi．Profiling of simultaneously vaulted and twisted blades theory,experiment,design and application[J]．Power Engineering,1992,12(6)：1-6(in Chinese)．
[11]
钟兢军．弯曲叶片控制扩压叶栅二次流动损失的实验研究[D]．哈尔滨：哈尔滨工业大学,1995． Zhong Jingjun．An experimental investigation by using curved blade to control secondary flow in compressor cascade[D]．Harbin：Harbin Institute of Technology,1995(in Chinese)．
[12]
杜鑫,焦映厚,张龙新,等．端弯控制扩压叶栅角区分离的机制分析[J]．中国电机工程学报,2014,34(2)：309-314． Du Xin,Jiao Yinghou,Zhang Longxin,et al．Mechanism study on the end-bend blade controlling the corner separation[J]．Proceedings of the CSEE,2014,34(2)：309-314(in Chinese)．
[13]
Du X,Wang S T,Wang Z Q．Study on the effect of End-bend cantilevered stator in a 2-stage axial compressor[J]．Journal of Thermal and Science,2009,18(2)：119-125．
[14]
杜鑫,王松涛,王仲奇,等．端弯联合弯叶片对扩压叶栅角区分离影响研究[J]．工程热物理学报,2012,33(10)：1687-1690． Du Xin,Wang Songtao,Wang Zhongqi,et al．Effects of endbend-bowed blade on corner separation of a diffusion cascade[J]．Journal of Engineering Thermophysics,2012,33(10)：1687-1690(in Chinese)．
[15]
张华良．采用叶片弯/掠及附面层抽吸控制扩压叶栅内涡结构的研究[D]．哈尔滨：哈尔滨工业大学工学博士学位论文,2007． Zhang Hualiang．Investigation on application of dihedral/swept blade and boundary layer suction to control vortex configuration in compressor cascades[D]．Harbin：Harbin Institute of Technology,2007(in Chinese)．
[16]
Zhang H L,Wang S T,Wang Z Q．Variation of vortex structure in a compressor cascade at different incidences[J]．Journal of Propulsion and Power,2007,23(1)：221-226．
[17]
Xing X Q,Zhou S,Zhao X L．Probing into the connotation of sweep aerodynamics of transonic fans and compressors[C]//American Society of Mechanical Engineers Turbomachinery Exposition,Louisiana,USA,2001-GT-0352,2001．
[18]
单鹏,桂幸民,周盛,等．高负荷后掠风扇设计若干基本问题[J]．工程热物理学报,1999,20(5)：576-579． Shan Peng,Gui Xingmin,Zhou Sheng,et al．Fundamental considerations on high loading backward swept fan design[J]．Journal of Engineering Thermophysics,1999,20(5)：576-579(in Chinese)．
[19]
邢秀清,单鹏,周盛．风扇转子前缘曲线相对掠对性能的影响[J]．航空动力学报,2000,15(1)：39-43． Xing Xiuqing,Shan Peng,Zhou Sheng．Effects of swept leading edge on performance of fans[J]．Journal of Aerospace Power,2005,15(1)：39-43(in Chinese)．
[20]
邹正平,赵令德,陈懋章,等．叶轮机叶片的三维造型及其对叶片气动负荷的影响[J]．航空动力学报,1998．13(3)：235-240． Zou Zhengping,Zhao Lingde,Chen Maozhang,et al．Three dimensional blading and its influence on blade aerodynamic loading[J]．Journal of Aerospace Power,1998,13(3)：235-240(in Chinese)．
