[SBH_]

Hello, I am trying to simulate the intake performance in a turbofan at climb conditions, where I have an AoA of 22 degrees. My domain is a box, where one face is set as inlet and the others as openings. At the inlet I specify my angle of attack by decomposing the velocity in Cartesian components, however as seen from the picture attached the direction of the flow comes back to axial direction downstream in the domain.

I have tried to rotate my mesh and kept constant the axial velocity, and also set more faces as inlets but nothing. Any suggestions??