| Citation: | Coherent structures of cascade under different attack angles with DMD method[J]. Journal of Aerospace Power, 2018, 33(9): 2150-2160. doi: 10.13224/j.cnki.jasp.2018.09.012
|
| [1] |
WANG Zhongnan,YUAN Xin.Unsteady mechanism of compressor corner separation over a range of incidence based on hybrid LES/RANS［R］.ASME Paper GT2013-95300,2013.
|
| [2] |
PULLAN G,YOUNG A M,DAY I J,et al.Origins and structure of spike-type rotating stall［R］.ASME Paper GT2012-68707,2012.
|
| [3] |
YAMADA K,FURUKAWA M,TAMURA Y,et al.Large-scale DES analysis of stall inception process in a multi-stage axial flow compressor［R］.ASME Paper GT2016-57104,2016.
|
| [4] |
宋彦萍,刘振德,陈浮,等.采用弯-掠叶片的压气机叶栅变冲角性能研［J］.推进技术,2004,25(5):411-415.SONG Yanping,LIU Zhende,CHEN Fu,et al.Investigation of swept and curved compressor cascade performance under different incidences［J］.Journal of Propulsion Technology,2004,25(5):411-415.(in Chinese)
|
| [5] |
SWIICHI I,MASATO F,KENICHIRO I,et al.Vortical flow structure and loss generation process in a transonic centrifugal compressor impeller［R］.ASME Paper GT2007-27791,2007.
|
| [6] |
刘若阳,侯安平,单树军,等.基于DDES方法的叶栅分离旋涡的非定常流动数值研究［J］.推进技术,2017,38(1):16-26.LIU Ruoyang,HOU Anping,SHAN Shujun,et al.Unsteady numerical investigation on cascade separation vortex flow based on delayed detached-eddy simulation［J］.Journal of Propulsion Technology,2017,38(1):16-26.(in Chinese)
|
| [7] |
FENG Junhong,SHEN Chibing,WANG Qiancheng.Three-dimensional evolution of large-scale vortices in supersonic flow［J］.Applied Physics Letters,2015,107(25):453-477.
|
| [8] |
史万里.涡轮流场大涡模拟与拟序结构研究［D］.南京：南京航空航天大学,2012.SHI Wanli.Investigation of large eddy simulation and coherent structure for the flow field of turbine vane［D］.Nanjing:Nanjing University of Aeronautics and Astronautics,2012.(in Chinese)
|
| [9] |
DENNIS D J C,NICKELS T B.Experimental measurement of large-scale three-dimensional structures in a turbulent boundary layer:Part Ⅰ vortex packets［J］.Journal of Fluid Mechanics,2011,673(4):180-217.
|
| [10] |
FENG Liaho,WANG Jinjun,PAN Chong.Proper orthogonal decomposition analysis of vortex dynamics of a circular cylinder under synthetic jet control［J］.Physics of Fluids,2011,23(1):014106.1-014106.13.
|
| [11] |
朱剑锋,黄国平,傅鑫,等.基于POD方法的弯曲扩压通道分离流控制的时空特性分析［J］.航空学报,2014,35(4):921-932.
ZHU Jianfeng,HUANG Guoping,FU Xin,et al.Spatiotemporal characteristics analysis for controlling flow separation in divergent curved channels with POD method［J］.Acta Aeronautica et Astronautica Sinica,2014,35(4):921-932.(in Chinese) |
| [12] |
MEZIC I.Analysis of fluid flows via spectral properties of Koopman operator［J］.Annual Review of Fluid Mechanics,2013,45(1):357-378.
|
| [13] |
ZHANG Qingshan,LIU Yingzheng,WANG Shaofei.The identification of coherent structures using proper orthogonal decomposition and dynamic mode decomposition［J］.Journal of Fluids and Structures,2014,49(8):53-72.
|
| [14] |
ROWLEY C,MEZIC I,BAGHERI S,et al.Spectral analysis of nonlinear flows［J］.Journal of Fluid Mechanics,2009,641:115-127.
|
| [15] |
SCHMID P.Dynamic mode decomposition of numerical and experimental data［J］.Journal of Fluid Mechanics,2010,656(10):5-28.
|
| [16] |
SEMLITSCH B,MIHAESCU M.Flow phenomena leading to surge in a centrifugal compressor［J］.Energy,2016,103(C):572-587.
|
| [17] |
洪树立,黄国平.引入DMD方法研究有/无控气流分离的动态结构［J］.航空学报,2017,38(8):10-17.HONG Shuli,HUANG Guoping.Introduce DMD method to study the dynamic structures of flow separation with and without control［J］.Acta Aeronautica et Astronautica Sinica,2017,38(8):10-17.(in Chinese)
|
| [18] |
胡骏,吴铁鹰,曹人靖.航空叶片机原理［M］.北京:国防工业出版社,2006.
|
| [19] |
朱剑锋,黄国平,傅鑫,等.无源微脉冲射流抑制叶栅气流分离的初步实验［J］.航空动力学报,2014,29(2):391-397.ZHU Jianfeng,HUANG Guoping,FU Xin,et al.Preliminary experiment of suppressing flow separation in cascade by micro pulsed jet without external device［J］.Journal of Aerospace Power,2014,29(2):391-397.(in Chinese)
|
| [20] |
朱剑锋.脉冲射流抑制大扩压度压气机流动分离的机理及方法研究［D］.南京：南京航空航天大学,2013.ZHU jianfeng.Method and mechanism investigation of reducing flow separation in large diffusion compressors by pulsed jet［D］.Nanjing:Nanjing University of Aeronautics and Astronautics,2013.(in Chinese)
|
| [21] |
TU J,ROWLEY C,ARAME,et al.Koopman spectral analysis of separated flow over a finite-thickness flat plate with elliptical leading edge［R］.AIAA 2011-38,2011.
|
| [22] |
GURSUL I,WANG Z,VARDDAKI E.Review of flow control mechanisms of leading-edge vortices［J］.Progress in Aerospace Sciences,2007,43(7):246-270.
|
| [23] |
SEIFERT A,BACHAR T,KOSS D,et al.Oscillatory blowing:a tool to delay boundary-layer separation［J］.AIAA Journal,1993,31(11):2052-2060.
|
| [24] |
SEIFERT A,PACK L .Oscillatory control of separation at high Reynolds numbers［J］.AIAA Journal,2012,37(9):1062-1071.
|
| [25] |
GREENBLATT D,WYGNANSKI I.Parameters affecting dynamic stall control by oscillatory excitation［R］.AIAA-93-3121,1993.
|
| [26] |
PACK L,SCHAEFFLER N,YAO C,et al.Active control of flow separation from the slat shoulder of a supercritical airfoil［R］.AIAA 2002-3156,2002.
|
| [27] |
颜超,陆小庆,郑琴.EOF、SVD和POD的数学统一［J］.数学的实践与认识,2014,44(22):236-242.YAN Chao,LU Xiaoqing,ZHENG Qin.The mathematical unification of EOF,SVD and POD［J］.Mathematics in Practice and Theory,2014,44(22):236-242.(in Chinese)
|
DownLoad: