[bharathlatchireddi]

I'm encountering an issue with my CFD analysis on a Fixed-wing VTOL with a pusher propeller. Specifically, I'm trying to understand the impact of the pusher propeller on the airflow around the rear wing. The rotor domain within the outer domain is mistakenly identified as walls, which I suspect is causing inaccuracies in my lift and drag calculations compared to XFLR results. Despite achieving convergence after over 7000 iterations in ANSYS FLUENT, the problem persists. If anyone has experience with this type of issue, your insights would be greatly appreciated. Thank you.