An approach to wall modeling in large-eddy simulations

被引:322
|
作者
Nikitin, NV
Nicoud, F
Wasistho, B
Squires, KD
Spalart, PR
机构
[1] Boeing Commercial Airplanes, Seattle, WA 98124 USA
[2] Russian Acad Sci, Inst Appl Mech, Moscow 117334, Russia
[3] Stanford Univ, Ctr Turbulence Res, Stanford, CA 94305 USA
[4] Arizona State Univ, Dept Mech & Aerosp Engn, Tempe, AZ 85287 USA
[5] CERFACS, F-31057 Toulouse, France
关键词
D O I
10.1063/1.870414
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Channel flow with friction Reynolds number Re-tau as high as 80 000 is treated by large-eddy simulation at a moderate cost, using the subgrid-scale model designed for detached-eddy simulations. It includes wall modeling, and was not adjusted for this flow. The grid count scales with the logarithm of the Reynolds number. Three independent codes are in fair agreement with each other. Reynolds-number variations and grid refinement cause trades between viscous, modeled, and resolved shear stresses. The skin-friction coefficient is too low, on the order of 15%. The velocity profiles contain a "modeled" logarithmic layer near the wall and some suggest a "resolved" logarithmic layer farther up, but the two layers have a mismatch of several units in U+. (C) 2000 American Institute of Physics. [S1070-6631(00)01607-X].
引用
收藏
页码:1629 / 1632
页数:4
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