Wall model for large-eddy simulation based on the lattice Boltzmann method

被引:61
作者
Malaspinas, O. [1 ,2 ]
Sagaut, P. [1 ]
机构
[1] Univ Paris 06, Inst Jean Rond Alembert, UMR 7190, F-75252 Paris, France
[2] Univ Geneva, Ctr Univ Informat, CH-1227 Geneva, Switzerland
基金
瑞士国家科学基金会;
关键词
Lattice Boltzmann method; Large-eddy simulation; Boundary layer; Wall modeling; Subgrid modeling; Turbulent plane channel; BOUNDARY-CONDITIONS; FLOW; SCHEMES;
D O I
10.1016/j.jcp.2014.06.020
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
An original wall-model for lattice Boltzmann based large-eddy simulation is presented. It relies on either an analytical profile for the velocity profile within the first off-wall cell or the solution of Turbulent Boundary Layer Equations. The latter are solved thanks to a meshless approach to obtain a user-friendly method. The proposed method is observed to be both robust and accurate, yielding very satisfactory results in plane channel flow up to R-et = 20000 on uniform grids with Delta x(+) = Delta y(+) = Delta z(+) = 1000. The computed maximum error on skin friction is about 4% in most investigated cases on the coarsest grids (10 grid points across the half-channel height). It lies within 1-2% on finer grids with 20-60 uniformly distributed grid points in the channel half-height. (C) 2014 Elsevier Inc. All rights reserved.
引用
收藏
页码:25 / 40
页数:16
相关论文
共 58 条
[1]   Lattice-Boltzmann Method for Complex Flows [J].
Aidun, Cyrus K. ;
Clausen, Jonathan R. .
ANNUAL REVIEW OF FLUID MECHANICS, 2010, 42 :439-472
[2]  
[Anonymous], 2013, LARGE EDDY SIMULATIO
[3]  
[Anonymous], 2006, LARGE EDDY SIMULATIO
[4]   Two-layer approximate boundary conditions for large-eddy simulations [J].
Balaras, E ;
Benocci, C ;
Piomelli, U .
AIAA JOURNAL, 1996, 34 (06) :1111-1119
[5]   Temperature wall modelling for large-eddy simulation in a heated turbulent plane channel flow [J].
Benarafa, Y. ;
Clonia, O. ;
Ducros, F. ;
Sagaut, P. .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2007, 50 (21-22) :4360-4370
[6]   RANS/LES coupling for unsteady turbulent flow simulation at high Reynolds number on coarse meshes [J].
Benarafa, Y ;
Cioni, O ;
Ducros, F ;
Sagaut, P .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2006, 195 (23-24) :2939-2960
[7]   A MODEL FOR COLLISION PROCESSES IN GASES .1. SMALL AMPLITUDE PROCESSES IN CHARGED AND NEUTRAL ONE-COMPONENT SYSTEMS [J].
BHATNAGAR, PL ;
GROSS, EP ;
KROOK, M .
PHYSICAL REVIEW, 1954, 94 (03) :511-525
[8]   A compressible wall model for large-eddy simulation with application to prediction of aerothermal quantities [J].
Bocquet, S. ;
Sagaut, P. ;
Jouhaud, J. .
PHYSICS OF FLUIDS, 2012, 24 (06)
[9]   Momentum transfer of a Boltzmann-lattice fluid with boundaries [J].
Bouzidi, M ;
Firdaouss, M ;
Lallemand, P .
PHYSICS OF FLUIDS, 2001, 13 (11) :3452-3459
[10]   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