[bandecot]

Hi, I'm trying to simulate the efficiency of stabilizers of a airplain. Basically my geometry consists: fuselage, stabilizers and propeller.
I want to put a circle inlet to emulate the propeller on the nose of the airplane.
I know it's not the right way to do this, I should go for a unsteady analysis, but because of the computacional cost it's not possible in the moment.
I want to plot the streamlines with seed in the propeller and see how the flow affects the tail, I tried to create the propeller as a surface on Solid Works and set as an inlet on Star but it didn't work.

Should I create a body instead? Wich boundary conditions in the surfaces? If someone could help me I'll be glad, Thanks! Unfortunately I cannot send you the images.