Hello together,
I would like to evaluate the aerodynamic properties of an object with hyperworks cfd and the FarField condition. In order to use this type of boundary condition my simulation domain must be relatively big. To cut simulation time as much as possible I would like to apply a gradient to my mesh. That means that at the center of my domain (where the object is placed) I need a fine mesh while at the boundary of the domain the mesh can be much more coarse. Is there any way to achieve this with hyperworks or do I need an external meshing software. I have tried to apply different surface mesh densities to my object and the FarField surface but that has not worked.
A good representation of the mesh can be obtained here:
https://2021.help.altair.com/2021.2/hwsolvers/acusolve/topics/acusolve/turbulent_flow_over_a_naca_airfoil.htm
Best regards
Christoph