Boundary conditions for Helicopter Blade
I want to simualte the flow over Helicopter balde. In experiment there are two blades so I took one to model and apply the periodic conditions. Next I specified Fluid as a moving reference frame (I am not sure about that) and wall also moving (but with zero velocity). The next thing is that I applied Pressure outlet on all of the outside domain.
Can anybody tell me that are my boundary conditions correct?
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