Andre Weiner, Institute of Fluid Mechanics
properties of turbulent scales
large scales
small scales
LES core idea: resolve large structures and model influence of smallest structures
How is the turbulence kinetic energy affected?
topics in LES modeling
filtering in 3D, no boundaries
$$ \widetilde{\varphi} (\mathbf{x}) = \int_{\mathbb{R}^3} G(\mathbf{x}, \mathbf{y}, \Delta (\mathbf{x}))\ \varphi (\mathbf{x}) \mathrm{d}\mathbf{y} $$
$$ \int_{\mathbb{R}^3} G(\mathbf{x}, \mathbf{y}, \Delta (\mathbf{x})) \mathrm{d}\mathbf{y} = 1 $$
$\Delta $ - filter width, $G$ - filter function
3D expressed as 1D filtering
$$ G(\mathbf{x}, \mathbf{y}, \Delta (\mathbf{x})) = \prod_{i=x,y,z} G_i(x_i, y_i, \Delta_i (x_i)) $$
typical filters for theoretical analysis
some mathematical properties of filtering
derivation of filtered momentum and mass conservation equation
further aspects
SGS model overview
additional stochastic and dynamic variants
brief historical perspective
eddy viscosity approach
$$\tau_{ij} = \widetilde{u_iu_j} - \widetilde{u_i}\widetilde{u_j}$$
$$\tau_{ij}^{mod} = -2\nu_t\widetilde{S}_{ij} + \frac{1}{3}\delta_{ij}\tau_{kk}$$
$\rightarrow$ similar advantages and shortcomings as in RANS approach but typically less pronounced
Prandtl's mixing length idea for $\nu_t$
$$\nu_t = l_c u_c$$
$l_c := f(\Delta)$ (in contrast to RANS)
typical choice $\Delta = V^{1/3}$
$\rightarrow$ only $u_c$ needed
$\nu_t$-based SGS models
some (rough) guidelines for meshing - wall-resolved LES
How to deal with inflow BCs in reduced domains?