Dynamic non-equilibrium wall-modeling for large eddy simulation at high Reynolds numbers

被引:119
作者
Kawai, Soshi [1 ]
Larsson, Johan [2 ]
机构
[1] Japan Aerosp Explorat Agcy, Inst Space & Aeronaut Sci, Chuo Ku, Sagamihara, Kanagawa 2525210, Japan
[2] Univ Maryland, Dept Mech Engn, College Pk, MD 20742 USA
基金
日本学术振兴会;
关键词
DIRECT NUMERICAL-SIMULATION; SUBGRID-SCALE MODEL; BOUNDARY-LAYER; TURBULENCE;
D O I
10.1063/1.4775363
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A dynamic non-equilibrium wall-model for large-eddy simulation at arbitrarily high Reynolds numbers is proposed and validated on equilibrium boundary layers and a non-equilibrium shock/boundary-layer interaction problem. The proposed method builds on the prior non-equilibrium wall-models of Balaras et al. [AIAA J. 34, 1111-1119 (1996)] and Wang and Moin [Phys. Fluids 14, 2043-2051 (2002)]: the failure of these wall-models to accurately predict the skin friction in equilibrium boundary layers is shown and analyzed, and an improved wall-model that solves this issue is proposed. The improvement stems directly from reasoning about how the turbulence length scale changes with wall distance in the inertial sublayer, the grid resolution, and the resolution-characteristics of numerical methods. The proposed model yields accurate resolved turbulence, both in terms of structure and statistics for both the equilibrium and non-equilibrium flows without the use of ad hoc corrections. Crucially, the model accurately predicts the skin friction, something that existing non-equilibrium wall-models fail to do robustly. (C) 2013 American Institute of Physics. [http://dx.doi.org/10.1063/1.4775363]
引用
收藏
页数:21
相关论文
共 35 条
[1]  
[Anonymous], 2006, THESIS U TOKYO
[2]   Two-layer approximate boundary conditions for large-eddy simulations [J].
Balaras, E ;
Benocci, C ;
Piomelli, U .
AIAA JOURNAL, 1996, 34 (06) :1111-1119
[3]   Approximate wall boundary conditions in the large-eddy simulation of high reynolds number flow [J].
Cabot, W ;
Moin, P .
FLOW TURBULENCE AND COMBUSTION, 2000, 63 (1-4) :269-291
[4]   COMPUTATIONAL AERODYNAMICS DEVELOPMENT AND OUTLOOK [J].
CHAPMAN, DR .
AIAA JOURNAL, 1979, 17 (12) :1293-1313
[5]   Grid-point requirements for large eddy simulation: Chapman's estimates revisited [J].
Choi, Haecheon ;
Moin, Parviz .
PHYSICS OF FLUIDS, 2012, 24 (01)
[6]   A NUMERICAL STUDY OF 3 DIMENSIONAL TURBULENT CHANNEL FLOW AT LARGE REYNOLDS NUMBERS [J].
DEARDORFF, JW .
JOURNAL OF FLUID MECHANICS, 1970, 41 :453-+
[7]   Reynolds-number scaling of the flat-plate turbulent boundary layer [J].
DeGraaff, DB ;
Eaton, JK .
JOURNAL OF FLUID MECHANICS, 2000, 422 :319-346
[8]   Pade-type higher-older boundary filters for the Navier-Stokes equations [J].
Gaitonde, DV ;
Visbal, MR .
AIAA JOURNAL, 2000, 38 (11) :2103-2112
[9]  
Grotzbach G., 1987, Encyclopedia of Fluid Mechanics ed
[10]   EVALUATION OF THEORIES FOR PREDICTING TURBULENT SKIN FRICTION AND HEAT TRANSFER ON FLAT PLATES AT SUPERSONIC AND HYPERSONIC MACH NUMBERS [J].
HOPKINS, EJ ;
INOUYE, M .
AIAA JOURNAL, 1971, 9 (06) :993-&