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 | ✓ | ✓ |
inflow direction | ✓ | ✓ |
static temperature | ✓ | ✓ |
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
- static pressure
- static temperature
Incompressible and Compressible Equation of State
The boundary face velocity is assigned the specified velocity at the boundary:
The static pressure is extrapolated from the static pressure at the interior of the domain:
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:
- Outflow
- Under outflow conditions, the face value of static temperature is extrapolated from the adjacent cell:
The density and the total enthalpy are calculated as: