Large-eddy simulation of the zero pressure gradient, turbulent boundary layer

ORAL

Abstract

Large-eddy simulations (LES) of the zero-pressure gradient, smooth-wall, flat-plate turbulent boundary layer are presented. The LES combines the stretched-vortex, subgrid-scale (SGS) model with a tailored, near-wall model designed to incorporate anisotropic vorticity scales in the presence of the wall. Specifically, an approximate analytic integration of the stream-wise momentum equation across the near-wall layer, with inner-scaling used to reduce inertial terms, leads to a hyperbolic partial differential equation for the wall shear stress. This is coupled to an SGS model of streamwise, attached vortices in the presence of the wall, constructed to capture the principal dynamical behavior of longitudinal vortices in wall-normal transport of streamwise momentum. The result is an effective slip-velocity boundary condition for the LES at a raised ``virtual wall'' together with a dynamical calculation of the K\'arm\'an constant. Presently we demonstrate LES of the spatially developing, turbulent boundary layer at Reynolds numbers $Re_\theta$ based on the free-stream velocity and the momentum thickness in the range $Re_\theta = 10^3 -10^{12}$. At large $Re_\theta$, the calculated skin-friction coefficient agrees well with the Coles-Fernholz relation.

Authors

  • Michio Inoue

    Caltech

  • Dale Pullin

    Caltech, California Institute of Technology