Spalart–Allmaras turbulence model


The Spalart–Allmaras model is a one-equation model that solves a modelled transport equation for the kinematic eddy turbulent viscosity. The Spalart–Allmaras model was designed specifically for aerospace applications involving wall-bounded flows and has been shown to give good results for boundary layers subjected to adverse pressure gradients. It is also gaining popularity in turbomachinery applications.
In its original form, the model is effectively a low-Reynolds number model, requiring the viscosity-affected region of the boundary layer to be properly resolved.
The Spalart–Allmaras model was developed for aerodynamic flows. It is not calibrated for general industrial flows, and does produce relatively larger errors for some free shear flows, especially plane and round jet flows. In addition, it cannot be relied on to predict the decay of homogeneous, isotropic turbulence.
It solves a transport equation for a viscosity-like variable. This may be referred to as the Spalart–Allmaras variable.

Original model

The turbulent eddy viscosity is given by
The rotation tensor is given by
where d is the distance from the closest surface and is the norm of the difference between the velocity at the trip and that at the field point we are considering.
The constants are

Modifications to original model

According to Spalart it is safer to use the following values for the last two constants:
Other models related to the S-A model:
DES
DDES

Model for compressible flows

There are two approaches to adapting the model for compressible flows. In the first approach, the turbulent dynamic viscosity is computed from
where is the local density. The convective terms in the equation for are modified to
where the right hand side is the same as in the original model.

Boundary conditions

Walls:
Freestream:
Ideally, but some solvers can have problems with a zero value, in which case can be used.
This is if the trip term is used to "start up" the model. A convenient option is to set in the freestream. The model then provides "Fully Turbulent" behavior, i.e., it becomes turbulent in any region that contains shear.
Outlet: convective outlet.