Setting Boundary Conditions

Set the conditions at the boundaries of the airfoil and the domain.

The geometry used for this tutorial has only two boundaries for the physics:
  • A wall boundary representing the surface of the airfoil and defined in the Overset region.
  • A freestream boundary at the external edge of the entire solution domain defined in the Background region.
Set the freestream conditions on the outer perimeter of the Background region:
Edit the Regions > Background 2D > Boundaries > Outside > Physics Values node and set the following properties:
Node Property Setting
Mach Number Value 0.725
Static Temperature Value 300 K

All other conditions for the freestream boundary and the default wall are suitable for this problem.