| Citation: | YANG Hui, SHEN Zhen, ZHENG Yun. Influence of blade untwist on transonic high bypass ratio fan performance[J]. Journal of Aerospace Power, 2016, 31(1): 100-105. doi: 10.13224/j.cnki.jasp.2016.01.014
|
| [1] |
陈懋章,刘宝杰.风扇/压气机气动设计技术发展趋势-用于大型客机的大涵道比涡扇发动机[J].航空动力学报,2008,23(6):961-975. CHEN Maozhang,LIU Baojie.Fan/compressor aero design trend and challenge on the development of high bypass ratio turbofan[J].Journal of Aerospace Power,2008,23(6):961-975.(in Chinese)
|
| [2] |
宋兆鸿,熊昌炳,郑光华.航空燃气涡轮发动机强度设计[M].北京:北京航空航天大学出版社,1988.
|
| [3] |
陈懋章,刘宝杰.大涵道比涡扇发动机风扇/压气机气动设计技术分析[J].航空学报,2008,29(3):513-526. CHEN Maozhang,LIU Baojie.Fan/compressor aero design technology for high bypass ratio turbofan[J].Acta Aeronautica et Astronautica Sinica,2008,29(3):513-526.(in Chinese)
|
| [4] |
Wilson M J,Imregun M,Sayma A I.The effect of stagger variability in gas turbine fan assemblies[J].Journal of Turbomachinery,2007,129(2):404-411.
|
| [5] |
Kallesøe B S,Hansen M H.Some effects of large blade deflections on aeroelastic stability[R].AIAA-2009-839,2009.
|
| [6] |
Roehle I,Le Guevel A,Fradin C.3D-shock visualisation in a transonic compressor rotor[J].Optics and Laser Technology,1999,31(1):67-73.
|
| [7] |
Yamamoto O,August R.Structural and aerodynamic analysis of a large-scale advanced propeller blade[J].Journal of Propulsion and Power,1992,8(2):367-373.
|
| [8] |
Kaza K R V,Mehmed O,Narayanan G V,et al.Analytical flutter investigation of a composite propfan model[R].AIAA 87-0738,1987.
|
| [9] |
Srivastava R,Sankar L N,Reddy T S R,et al.Application of an efficient hybrid scheme for aeroelastic analysis of advanced propellers[J].Journal of Propulsion and Power,1991,7(5):767-775.
|
| [10] |
廖伟丽,许斌,逯鹏,等.部分负荷下混流式水轮机转轮叶片变形对流场的影响[J].机械工程学报,2006,42(6):55-59. LIAO Weili,XU Bin,LU Peng,et al.Influence of runner blade deformation on fluid field of francis turbine under part load[J].Chinese Journal of Mechanical Engineering,2006,42(6):55-59.(in Chinese)
|
| [11] |
王宏亮,席光.离心叶轮几何形变对气动性能的影响[J].西安交通大学学报,2009,43(5):46-50. WANG Hongliang,XI Guang.Influence of centrifugal blade deformation on impeller aerodynamic performance[J].Journal of Xi'an Jiaotong University,2009,43(5):46-50.(in Chinese)
|
| [12] |
LIU Gaolian.The generalized untwist problem of rotating blades:a coupled aeroelastic formulation[J].International Journal of Turbo and Jet Engines,1995,12(2):109-117.
|
| [13] |
封卫兵,何吉欢,刘高联.大变形耦合热弹性动力学的变分原理[J].上海交通大学学报,2001,35(4):614-617. FENG Weibing,HE Jihuan,LIU Gaolian.Variational principles for coupled thermoelasticity with finite dispalcement[J].Journal of Shanghai Jiaotong University,2001,35(4):614-617.(in Chinese)
|
| [14] |
Sadeghi M,Liu F.Coupled fluid-structure simulation for turbomachinery blade rows[R].AIAA-2005-0018,2005.
|
| [15] |
郑赟.基于非结构网格的气动弹性数值方法研究[J].航空动力学报,2009,24(9):2069-2077. ZHENG Yun.Computational aeroelasticity with an unstructured grid method[J].Journal of Aerospace Power,2009,24(9):2069-2077.(in Chinese)
|
| [16] |
郑赟,田晓,杨慧.跨声速风扇叶片变形对气动性能的影响[J].航空动力学报,2011,26(7):1621-1627. ZHENG Yun,TIAN Xiao,YANG Hui.Impact of blade deflection on aerodynamic performance of a transonic fan[J].Journal of Aerospace Power,2011,26(7):1621-1627.(in Chinese)
|
| [17] |
郑赟,王彪,杨慧.跨声速风扇叶片的反扭设计研究[J].机械工程学报,2013,49(5):147-153. ZHENG Yun,WANG Biao,YANG Hui.Numerical study on blade unrunning design of a transonic fan[J].Journal of Mechanical Engineering,2013,49(5):147-153.(in Chinese)
|
| [18] |
郑赟,王彪,王静,等.多块协调变形的网格变形技术及其应用[J].航空计算技术,2012,42(1):83-87. ZHENG Yun,WANG Biao,WANG Jing,et al.Mesh deforming technique based on compatibility of multi-block structured mesh deformation and its application to blade aeroelastic analysis in turbomachinery[J].Aeronautical Computing Technique,2012,42(1):83-87.(in Chinese)
|
DownLoad: