I am working on a CFD analysis of blended wing body aircraft. In the following geometry, I pretend to simulate deflection of a central rudder at specific angle, 5º. In this case, the mesh has problems in the intersection between the fixed rudder and deflected rudder. I have tried to solve, but I get high levels of non-orthogonality yet.
The non-orthogonality is around 80, if I couldn’t decrease this value, could I realise my simulation although the non-orthogonality is higher than 75, the recommended value?
Any suggestion about how improve my geometry or add new regions at mesh?