Symmetry Plane

A symmetry plane boundary represents an imaginary plane of symmetry in the simulation. You can use the symmetry plane boundary condition to reduce the extent of the computational domain in locations where the geometry and the flow are symmetric. The symmetry plane boundary can also be used as a planar "slip wall" with the shear stress being zero.

Boundary Inputs

For a symmetry plane boundary, you specify no conditions.

Computed Values

The symmetry plane boundary condition is valid for incompressible and compressible flows. Simcenter STAR-CCM+ computes the following values at the boundary faces:

  • velocity v
  • static pressure Ps
  • static temperature Ts

Incompressible and Compressible Equation of State

The symmetry plane is a boundary surface on which the normal velocity and the normal gradient of all other variables are zero. Consequently, there is zero flux across the symmetry plane boundary.

The tangential shear stress at a symmetry boundary is zero. The face value of velocity is computed by extrapolating the velocity in the adjacent cell using reconstruction gradients and subtracting the normal velocity:

Figure 1. EQUATION_DISPLAY
v=vext(vextn)n
(833)

where the superscript ext indicates that the value is extrapolated from the adjacent cell and n=a/|a| with a being the outward pointing face area vector.

The boundary face value for static pressure is extrapolated from the adjacent cell:

Figure 2. EQUATION_DISPLAY
Ps=Psext
(834)

For non-isothermal cases, the boundary face value for static temperature is given as:

Figure 3. EQUATION_DISPLAY
Ts=Tsext
(835)