Hi,
I am trying to simulate an aerofoil at different AOA. I simulated the aerofoil at 0 deg of aoa. But I couldn’t do it correctly in aoa at 8 deg. I set the same setting and I run simulation, but the results are coming wrong. Especially the flow direction is coming wrong way. I could’t able to understand where I am making mistake. Can you help me to find the mistake?
Regards,
Dinesh.