Hi,
I am working on a 2D wing simulation. I drew a convexe profile and I want to mesh it before computing a tuburlent flow SST phyisic. I have troubles with my solutions convergence and I think it is because of my mesh. I followed the tutorial "flow around an inclined NACA" but I need a more precise mesh for my profile. I tried to make it finer but it didn't work. That is why I want to sudivide my profil to make different domains (by adding points ?) like in the attached file.
Do you think it will resolve my problem ? How can I do such sbidivisions along my profil ?
Thank you,
Best regards,
Julien