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Theory for the Pressure, No Viscous Stress Boundary Condition

The Turbulent intensity IT, Turbulence length scale LT, and Reference velocity scale Uref values are related to the turbulence variables via

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

3

 

 

 

 

 

 

 

 

 

 

 

 

C3 4

 

2

--

k

=

3

I

 

U

 

 

2

,

 

=

3 ITUref

2

2--

T

ref

 

---L----T-----

 

-------------2-----------

---

 

 

 

 

 

 

 

 

 

 

 

 

 

For recommendations of physically sound values see Inlet Values for the

Turbulence Length Scale and Intensity.

See Also

The Inflow and Outflow feature options are available with the Inlet and Outlet Boundary conditions.

Theory for the Laminar Inflow Condition

In order to prescribe an inlet velocity profile, this boundary condition adds a weak form contribution corresponding to one-dimensional Navier-Stokes equations projected on the boundary. The applied condition corresponds to the situation shown in Figure 4-2: a fictitious domain of length Lentr is assumed to be attached to the inlet of the computational domain. This boundary condition uses the assumption that flow in this fictitious domain is a laminar plug flow. If the option is selected that constrains outer edges or endpoints to zero, the assumption is instead that the flow in the fictitious domain is fully developed laminar channel flow (in 2D) or fully developed laminar internal flow (in 3D). This does not affect the boundary condition in the real domain, , where the boundary conditions are always fulfilled.

pentr

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Lentr

Figure 4-2: Example of the physical situation simulated when using the Laminar inflow boundary condition. is the actual computational domain while the dashed domain is a fictitious domain.

136 | C H A P T E R 4 : S I N G L E - P H A S E F L O W B R A N C H

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