Cebeci–Smith Model
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The Cebeci–Smith model, developed by Tuncer Cebeci and Apollo M. O. Smith in 1967, is a 0-equation
eddy viscosity Viscosity is a measure of a fluid's rate-dependent drag (physics), resistance to a change in shape or to movement of its neighboring portions relative to one another. For liquids, it corresponds to the informal concept of ''thickness''; for e ...
model used in
computational fluid dynamics Computational fluid dynamics (CFD) is a branch of fluid mechanics that uses numerical analysis and data structures to analyze and solve problems that involve fluid dynamics, fluid flows. Computers are used to perform the calculations required ...
analysis of
turbulence In fluid dynamics, turbulence or turbulent flow is fluid motion characterized by chaotic changes in pressure and flow velocity. It is in contrast to laminar flow, which occurs when a fluid flows in parallel layers with no disruption between ...
in
boundary layer In physics and fluid mechanics, a boundary layer is the thin layer of fluid in the immediate vicinity of a Boundary (thermodynamic), bounding surface formed by the fluid flowing along the surface. The fluid's interaction with the wall induces ...
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, it is not suitable for large regions of
flow separation In fluid dynamics, flow separation or boundary layer separation is the detachment of a boundary layer from a surface into a wake. A boundary layer exists whenever there is relative movement between a fluid and a solid surface with viscous fo ...
and significant curvature or rotation. 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 = \begin _\text & \mbox y \le y_\text \\ _\text & \mbox y > y_\text \end where y_\text is the smallest distance from the surface where _\text is equal to _\text. The inner-region eddy viscosity is given by: : _\text = \rho \ell^2 \left left( \frac\right)^2 + \left(\frac\right)^2 \right where : \ell = \kappa y \left( 1 - e^ \right) with the von Karman constant \kappa usually being taken as 0.4, and with : A^+ = 26\left +y\frac\right The eddy viscosity in the outer region is given by: : _\text = \alpha \rho U_e \delta_v^* F_K where \alpha=0.0168, \delta_v^* is the displacement thickness, given by : \delta_v^* = \int_0^\delta \left(1 - \frac\right)\,dy and ''F''''K'' is the Klebanoff intermittency function given by : F_K = \left + 5.5 \left( \frac \right)^6 \right


References

* Smith, A.M.O. and Cebeci, T., 1967. ''Numerical solution of the turbulent boundary layer equations''. Douglas aircraft division report DAC 33735 * Cebeci, T. and Smith, A.M.O., 1974. ''Analysis of turbulent boundary layers''. Academic Press, * Wilcox, D.C., 1998. ''Turbulence Modeling for CFD''. , 2nd Ed., DCW Industries, Inc.


External links

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{{DEFAULTSORT:Cebeci-Smith model Turbulence models Fluid dynamics Mathematical modeling