Velocity Inlet

The velocity inlet boundary is usually used as an inflow condition where the distributions of velocity and fluid properties are known. At this inflow boundary, the conditions are prescribed and used to calculate the inlet volume flux as well as the fluxes of momentum and energy.

Boundary Inputs

For a velocity inlet boundary, you specify the following variables:

Inputs Incompressible Equation of State Compressible Equation of State (use only for subsonic compressible flow)
velocity vspec
inflow direction θspec
static temperature Ts,spec
The velocity vspec is specified with respect to a reference frame, which can be the laboratory, the region, or the local reference frame. The flow direction is either given as normal to the boundary, as individual angle components, or directly as flow direction angles.

Computed Values

The velocity inlet boundary condition is valid for incompressible and (subsonic) compressible flows. At the boundary, Simcenter STAR-CCM+ imposes or computes the following values, depending on the flow situation:

  • velocity v
  • static pressure Ps
  • static temperature Ts

Incompressible and Compressible Equation of State

The boundary face velocity is assigned the specified velocity at the boundary:

Figure 1. EQUATION_DISPLAY
v=vspecθspec
(780)

The static pressure Ps is extrapolated from the static pressure at the interior of the domain:

Figure 2. EQUATION_DISPLAY
Ps=Psext
(781)

For non-isothermal cases, the temperature at the boundary face is computed as follows:

Inflow
Under inflow conditions, the face value of static temperature is assigned the specified static temperature:
Figure 3. EQUATION_DISPLAY
Ts=Ts,spec
(782)
Outflow
Under outflow conditions, the face value of static temperature is extrapolated from the adjacent cell:
Figure 4. EQUATION_DISPLAY
Ts=Tsext
(783)

The density ρ and the total enthalpy Ht are calculated as:

Figure 5. EQUATION_DISPLAY
ρ=ρ(Ps,Ts)Ht=Hs(Ps,Ts)+v22
(784)