LES of the T106 low-pressure turbine: Spectral proper orthogonal decomposition of the flow based on a fluctuating energy norm

被引:5
作者
Fiore, M. [1 ]
Gojon, R. [1 ]
Saez-Mischlich, G. [1 ]
Gressier, J. [1 ]
机构
[1] Univ Toulouse, ISAE SUPAERO, Toulouse, France
关键词
Spectral proper orthogonal decomposition; Large-eddy simulation; T106 low-pressure turbine; LARGE-EDDY SIMULATION; MIXING LAYER; DNS; TRANSITION; CASCADE; BLADE; WAKES;
D O I
10.1016/j.compfluid.2022.105761
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
This paper investigates the use of the spectral proper orthogonal decomposition (SPOD) on the flow around the T106 low-pressure turbine cascade. The chosen metric of the SPOD is based on the hydrodynamic flow disturbances for compressible flows and is used to characterize the flow structures holding large energy disturbances and synchronization processes with incoming wakes when considered. The input data for the SPOD is provided by large-eddy simulations of the T106 cascade. The Reynolds number and free-stream turbulence effects on the flow structures are studied using four operating points investigated in previous experiments and numerical simulations: Reynolds numbers of Re = 5.18 x 104 and Re = 1.48 x 105 without and with upstream wakes. The analysis of the SPOD indicates that the upstream wakes can amplify some modes of the suction side boundary layer (apparently a receptivity mechanism) and intensify the developing blade wake turbulent structures downstream of the trailing edge. This amplification happens over a reduced frequency bandwidth between Strouhal numbers equal to 7-10 for the low Reynolds number case and 20-24 for the high Reynolds number case.
引用
收藏
页数:14
相关论文
共 35 条
  • [1] Spectral proper orthogonal decomposition and resolvent analysis of near-wall coherent structures in turbulent pipe flows
    Abreu, Leandra, I
    Cavalieri, Andre V. G.
    Schlatter, Philipp
    Vinuesa, Ricardo
    Henningson, Dan S.
    [J]. JOURNAL OF FLUID MECHANICS, 2020, 900
  • [2] Chu B.-T., 1965, Acta Mech, V1, P215
  • [3] Reconstruction of the global velocity field in the axisymmetric mixing layer utilizing the proper orthogonal decomposition
    Citriniti, JH
    George, WK
    [J]. JOURNAL OF FLUID MECHANICS, 2000, 418 : 137 - 166
  • [4] Unsteady boundary-layer transition in low-pressure turbines
    Coull, John D.
    Hodson, Howard P.
    [J]. JOURNAL OF FLUID MECHANICS, 2011, 681 : 370 - 410
  • [5] Numerical Study of Purge and Secondary Flows in a Low-Pressure Turbine
    Cui, Jiahuan
    Tucker, Paul
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2017, 139 (02):
  • [6] Numerical Investigation of Contrasting Flow Physics in Different Zones of a High-Lift Low-Pressure Turbine Blade
    Cui, Jiahuan
    Rao, V. Nagabhushana
    Tucker, Paul
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2016, 138 (01):
  • [7] Examination of large-scale structures in a turbulent plane mixing layer. Part 1. Proper orthogonal decomposition
    Delville, J
    Ukeiley, L
    Cordier, L
    Bonnet, JP
    Glauser, M
    [J]. JOURNAL OF FLUID MECHANICS, 1999, 391 : 91 - 122
  • [8] Broadband reconstruction of inhomogeneous turbulence using spectral proper orthogonal decomposition and Gabor modes
    Ghate, A. S.
    Towne, A.
    Lele, S. K.
    [J]. JOURNAL OF FLUID MECHANICS, 2020, 888
  • [9] Glauser M. N., 1987, TURBULENT SHEAR FLOW, P134, DOI DOI 10.1007/978-3-642-71435-113
  • [10] Large eddy simulation of flows in industrial compressors: a path from 2015 to 2035
    Gourdain, N.
    Sicot, F.
    Duchaine, F.
    Gicquel, L.
    [J]. PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2014, 372 (2022):