| Citation: | WANG Guojie, LIU Xuezheng, GAO Jie. Influence of form of tip gap on aerodynamic performance of centrifugal compressor using mixture of helium and xenon[J]. Journal of Aerospace Power, 2020, 35(6): 1304-1314. doi: 10.13224/j.cnki.jasp.2020.06.021
|
| [1] |
田志涛,郑群,姜斌.氦氙混合离心压气机设计与分析［J］.风机技术,2018,60(3):14-19. TIAN Zhitao,ZHENG Qun,JIANG Bin.Design and analysis of helium and xenon binary mixture gas centrifugal compressor［J］.Chinese Journal of Turbomachinery,2018,60(3):14-19.(in Chinese)
|
| [2] |
SKOCH G.Experimental investigation of centrifugal compressor stabilization techniques［J］.Journal of Turbomachinery,2003,125(4):765-776.
|
| [3] |
HAH C,KRAIN H.Secondary flows and vortex motion in a high-efficiency backswept impeller at design and off-design conditions［J］.Journal of Turbomachinery,1990,112(1):7-13.
|
| [4] |
MOORE J,MOORE J G.Secondary flow,separation and losses in the NACA 48-inch centrifugal impeller at design and off-design conditions［R］.ASME Paper 88-GT-101,1988.
|
| [5] |
SENOO Y.Mechanics on the tip clearance loss of impeller blades［J］.Journal of Turbomachinery,1991,113(4):680-685.
|
| [6] |
SENOO Y,ISHIDA M.Deterioration of compressor performance due to tip clearance of centrifugal impellers［J］.Transactions of the Japan Society of Mechanical Engineers,1987,109(1):55-61.
|
| [7] |
ISHIDA M,UEKI H,SENOO Y.Effect of blade tip configuration on tip clearance loss of a centrifugal impeller［J］.Transactions of the Japan Society of Mechanical Engineers,1990,112(1):14-18.
|
| [8] |
SCHLEER M,SONG S J,ABHARI A R S.Clearance effects on the onset of instability in a centrifugal compressor［J］.Journal of Turbomachinery,2006,130(3):993-1003.
|
| [9] |
SCHLEER M,ABHAEI R S.Clearance effects on the evolution of the flow in the vaneless diffuser of a centrifugal compressor at part load condition［J］.Journal of Turbomachinery,2008,130(3):031009.1-031009.9.
|
| [10] |
YAMADA K,TAMAGAWA Y,FUKUSHHIMA H,et al.Comparative study on tip clearance flow fields in two types of transonic centrifugal compressor impeller with splitter blades［R］.ASME Paper GT2010-23345,2010.
|
| [11] |
张楚华,王宝潼,栾辉宝,等.叶顶间隙对离心叶轮气动性能影响研究［J］.流体机械,2006,34(12):13-16. ZHANG Chuhua,WANG Baotong,LUAN Huibao,et al.Study on influence of tip clearance on aerodynamic performance of centrifugal impeller［J］.Fluid Machinery,2006,34(12):13-16.(in Chinese)
|
| [12] |
MASHIMO T,WATANABE I,ARIGA I.Effects of fluid leakage on performance of a centrifugal compressor［J］.Journal of Engineering for Gas Turbines and Power,1979,101(3):337-342.
|
| [13] |
楚武利,刘志伟.半开式离心叶轮间隙流动的实验研究［J］.流体机械,1998(10):3-6. CHU Wuli,LIU Zhiwei.Experimental study on clearance flow of semi open centrifugal impeller［J］.Fluid Machinery,1998(10):3-6.(in Chinese)
|
| [14] |
JAATINEN A,TURUNEN-SAARESTI T,GRNMAN A,et al.Experimental study of the effect of the tip clearance to the diffuser flow field and stage performance of a centrifugal compressor［R］.ASME Paper GT2012-68445,2012.
|
| [15] |
贾希诚,王正明,蔡睿贤.叶轮机械中叶顶间隙形态对气动性能影响的数值研究［J］.工程热物理学报,2001,22(4):431-434. JIA Xicheng,WANG Zhengming,CAI Ruixian.Numerical investigation of the effects of the tip gap shapes on aerodynamic performance in turbomachinery［J］.Journal of Engineering Thermophysics,2001,22(4):431-434.(in Chinese)
|
| [16] |
WEI C,GRATES D R,THERMANN H,et al.Numerical investigation of the influence of the tip clearance on wake formation inside a radial impeller［R］.ASME Paper GT2003-38279,2003.
|
| [17] |
冀国锋,桂幸民.轴流/离心压气机叶片通用任意中弧造型设计方法［J］.航空动力学报,2009,24(1):150-156. JI Guofeng,GUI Xingmin.A blading design method for axial/centrifugal compressor airfoils using arbitrary camber lines［J］.Journal of Aerospace Power,2009,24(1):150-156.(in Chinese)
|
| [18] |
冀国锋,殷明霞,桂幸民.某小型离心压气机气动设计［J］.航空动力学报,2010,25(3):557-564. JI Guofeng,YIN Mingxia,GUI Xingmin.Aerodynamic design of a small centrifugal compressor［J］.Journal of Aerospace Power,2010,25(3):557-564.(in Chinese)
|
DownLoad: