Observing Virtual Disk Meshing Requirements for the Body Force Propeller Method

It is recommended that you refine the mesh in the zone where the virtual disk is located, particularly in the radial direction. This way, you obtain a good distribution of the axial and tangential body force components of the virtual disk. If using the sampled velocity plane option, the grid on the upstream plane should match the grid on the virtual disk for optimal results.

For details on the body force computation, see Body Force Propeller Method.

The virtual disk (and inflow plane, where applicable) are marked on the mesh, during initialization, as per the user-specified values entered in the respective GUI. If you get a warning (server error), reporting that either the virtual disk or the inflow plane has no marked cells, then:
  • For the virtual disk, check the inputs set in the Disk Geometry node and make sure that the mesh is fine enough over the disk
  • For Inflow plane, try slightly increasing or decreasing the offset value used for the inflow velocity plane (or sampled velocity plane) as set in the [Inflow/Sampled] Velocity Plane node, to avoid alignment of the inflow plane with the mesh faces.
You can achieve a suitable mesh refinement by use of a volumetric control that is based on a cylindrical part shape, see Mesh Refinement In A Specified Volume. The diameter of the cylindrical part shape should correspond to the diameter of the inflow velocity plane. For more information, see Setting the Inflow Specification.

If you want to analyze the flow field in the wake of the propeller in more detail, refine the wake zone to a length of approximately fives times the virtual disk diameter.

NoteIf you set up a case from scratch—that is, the mesh is not yet available—it is recommended to first activate the virtual disk model, then specify the geometry and location of the virtual disk. Create the required volumetric controls for mesh refinement and then proceed with the meshing.