I am in the process of simulating a UAV propeller in a hover condition - therefore the inlet velocity is driven only by the suction of the propeller. I am simulating the propeller itself in a MRF zone. Incompressible, SIMPLE solver.
What are the correct boundary condition types to be used in the inlet and outlet in this case?
So far I am considering a pressureInletOutletVelocity for U inlet, and totalPressure for P inlet.
InletOutlet for V outlet, and fixedValue for P outlet.