Setting Boundary Conditions
Set the conditions at the boundaries of the airfoil and the domain.
- 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.
Edit the
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.