| Citation: | ZHU Haitao, LI Yan. High order direct numerical simulation of compressor cascade ,channel separated flow[J]. Journal of Aerospace Power, 2020, 35(6): 1286-1295. doi: 10.13224/j.cnki.jasp.2020.06.019
|
| [1] |
HORTON H P.Laminar separation bubbles in two-and three-dimensional incompressible flow［D］.London:University of London,1968.
|
| [2] |
PAULEY L L,MOIN P,REYNOLDS W C.The structure of two-dimensional separation［J］.Journal of Fluid Mechanics,1990,220:397-411.
|
| [3] |
SATYAM P,VIJAY M.Experimental study of flow through compressor cascade［J］.Case Studies in Thermal Engineering,2017,10:234-243.
|
| [4] |
钟兢军.弯曲叶片控制扩压叶栅二次流动的实验研究［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)
|
| [5] |
ZAKI T A,DURBIN P A,WISSINK J,et al.Direct numerical simulation of bypass and separation induced transition in a linear compressor cascade［R］.ASME Paper GT2006-90885,2006.
|
| [6] |
ZAKI T A,DURBIN P A,WU X.Separation and transition to turbulence in a compressor passage［R］.Palo Alto,US:Center for Turbulence Research,2006.
|
| [7] |
ZAKI T A,WISSINK P A,DURBIN W,et al.Direct computations of boundary layers distorted by migrating wakes in a linear compressor cascade［J］.Flow Turbulence Combustion,2009,83:307-322.
|
| [8] |
KANG S.An application of topological analysis to studying the three-dimensional flow in cascade Part Ⅰ:topological rules for skin-friction lines and section streamlines［J］.Applied Mathematics and Mechanics,1990,11(5):489-495.
|
| [9] |
GHERARDO Z,XAVIER O,JOCHEN K.Corner separation dynamics in a linear compressor cascade［J］.Journal of Fluids Engineering,2017,139:061101.1-061101.13.
|
| [10] |
王祥锋,颜培刚,俞李斌,等.两级轴流压气机流场内流动分离及旋涡运动［J］.空气动力学学报,2014,32(2):177-183. WANG Xiangfeng,YAN Peigang,YU Libin,et al.Flow separation and vortex motion in flow filed of two stage axial compressor［J］.Acta Aerodynamica Sinca,2014,32(2):177-183.(in Chinese)
|
| [11] |
LI R Y,GAO L M,ZHANG S,et al.Application of shear-sensitive liquid crystal coating to visualization of transition and reattachment in compressor cascade［J］.Chinese Journal of Aeronautics,2018,31(11):2073-2079.
|
| [12] |
WISSINK J G,RODI W,HODSON H P.The influence of disturbences carried by periodically incoming wakes on the separating flow around a turbine blade［J］.International Journal of Heat and Fluid Flow,2006,27:721-729.
|
| [13] |
LIU Y W,YAN H,LUI Y J,et al.Numerical study of corner separation in a linear compressor cascade using various turbulence models［J］.Chinese Journal of Aeronautics,2016,29(3):639-652.
|
| [14] |
RODI W.DNS and LES of some engineering flows［J］.Fluids Dynamics Research,2006,38(2/3):145-173.
|
| [15] |
RAI M M.A direct numerical simulation of transition and turbulence in a turbine stage［R］.AIAA 2009-584,2009.
|
| [16] |
WHEELER A P S,SANDBERG R D,SANDHAM N D,et al.Direct numerical simulation of a high-pressure turbine vane［J］.Journal of Turbomachinery,2016,138(7):071003.1-071003.9.
|
| [17] |
LIU C Q,WANG Y Q,YANG Y,et al.New omega vortex identification method［J］.Science China:Physics,Mechanics and Astronomy,2016,59(8):684711.1-684711.9.
|
| [18] |
肖志祥,罗堃宇,刘健.宽速域RANS-LES混合方法的发展及应用［J］.空气动力学学报,2017,35(3):338-353. XIAO Zhixiang,LUO Kunyu,LUI Jian.Development and applications of hybrid RANS/LES methods for wide-speed-range flows［J］.Acta Aerodynamica Sinca,2017,35(3):338-353.(in Chinese)
|
| [19] |
HILGENFELD L,PFITZNER M.Unsteady boundary layer development due to wake passing effects on a highly loaded linear compressor cascade［R］.ASME Paper 2004-GT-53186,2004.
|
| [20] |
ZHANG H D,WU Y,LI Y H,et al.Experimental investigation on a high subsonic compressor cascade flow［J］.Chinese Journal of Aeronautics,2015,28(4):1034-1043.
|
| [21] |
GHIA U,GHIA K N,SHIN C T.High-Re solutions for incompressible flow using the Navier-Stokes equations and a multigrid method［J］.Journal of Computational Physics,1982,48(3):387-411.
|
| [22] |
叶建.非定常环境中叶片边界层时空演化机制的大涡模拟［D］.北京:北京航空航天大学,2008.
|
DownLoad: