- Cebeci-Smith model
The Cebeci-Smith model is a 0-equation
eddy viscosity model used incomputational fluid dynamics analysis of turbulentboundary layer flows. The model gives eddy viscosity, , 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 theBaldwin-Lomax model , this model is not suitable for cases with large separated regions and significant curvature/rotation effects. Unlike theBaldwin-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:
:
where is the smallest distance from the surface where is equal to .
The inner-region eddy viscosity is given by:
:
where
:
with the von Karman constant usually being taken as 0.4, and with
:
The eddy viscosity in the outer region is given by:
:
where , is the
displacement thickness , given by:
and is the Klebanoff intermittency function given by
:
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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