[koalabryant]

Hi¡¡

I am simulating a 2d airfoil (Naca 64A010) and I got very good results with SST transitional mode, but as of 8º I got a bad cd compare to experimental results, as you can see in the picture I've uploaded.

I have tried almost everything but I can't get good results at high AoA.

Now I was wondering if it because in the experimental results they have an open trailing edge, and my simulation is with a closed trailing edge.

My parameters are
Re6e6
Transient, Step size: 0.001 Max iterations: 10
y+<1
C-Mesh 150000 cells (15c front x 20c back) orientating the back part of the mesh ~ half AoA


Thank you¡¡