Hi i need to run cfd and extract Cl Cd in diffrerent AoA. I'll attack all files (mesh, log).
This is my volume (chord is 1.56m and span is 0.143m) (aoa 0, vel 108.611 m/s)

Ill now attach the mesh condition specified

+

Now everithing seems fine till i plot Cp/chord. Crazy plts happens also when i plot lift and drag i have some points befor the "zero" of the x axis ??
and this are the data from acusolve cmd prompt

The mesh run took a couple of minutes but the solution run took 2.27 hours... and i got an intel i9 and 64gb of ram.
can u take a look guys and give me some advices, idk if im doing something wrong.
I'm looking foward to learn from u.
thank u all