Cebeci-Smith model

Cebeci-Smith model

The Cebeci-Smith model is a 0-equation eddy viscosity model used in computational fluid dynamics analysis of turbulent boundary layer flows. The model gives eddy viscosity, mu_t, as a function of the local boundary layer velocity profile. The model is suitable for high-speed flows with thin attached boundary-layers, typically present in aerospace applications. Like the Baldwin-Lomax model, this model is not suitable for cases with large separated regions and significant curvature/rotation effects. Unlike the Baldwin-Lomax model, this model requires the determination of a boundary layer edge.

Equations

In a two-layer model, the boundary layer is considered to comprise two layers: inner (close to the surface) and outer. The eddy viscosity is calculated separately for each layer and combined using:

:mu_t =egin{cases}{mu_t}_{inner} & mbox{if } y le y_{crossover} \ {mu_t}_{outer} & mbox{if } y > y_{crossover}end{cases}

where y_{crossover} is the smallest distance from the surface where {mu_t}_{inner} is equal to {mu_t}_{outer}.

The inner-region eddy viscosity is given by:

:{mu_t}_{inner} = ho l^2 l left [left( frac{partial U}{partial y} ight)^2 + left(frac{partial V}{partial x} ight)^2 ight] ^{1/2}

where

:l = kappa y left( 1 - e^{frac{-y^+}{A^+ ight)

with the von Karman constant kappa usually being taken as 0.4, and with

:A^+ = 26left [1+yfrac{dP/dx}{ ho u_ au^2} ight] ^{-1/2}

The eddy viscosity in the outer region is given by:

:{mu_t}_{outer} = alpha ho U_e delta_v^* F_{K}

where alpha=0.0168, delta_v^* is the displacement thickness, given by

:delta_v^* = int_0^delta (1-U/U_e)dy

and F_{K} is the Klebanoff intermittency function given by

:F_{K} = left [1 + 5.5 left( frac{y}{delta} ight)^6 ight] ^{-1}

References

* Smith, A.M.O. and Cebeci, T., 1967. "Numerical solution of the turbulent boundary layer equations". Douglas aircraft division report DAC 33735
* Wilcox, D.C., 1998. "Turbulence Modeling for CFD". ISBN 1-928729-10-X, 2nd Ed., DCW Industries, Inc.

External links

* This article was based on the [http://www.cfd-online.com/Wiki/Cebeci-Smith_model Cebeci Smith model] article in [http://www.cfd-online.com/Wiki CFD-Wiki]


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