Mesh problem for a compressible flow over an airfoil (NACA)

Hi again @atalavera_diez,

just to give you some feedback regarding your project:

  • I would suggest increasing the domain size vertically and have the mesh refinement more in the area of the pressure fronts.

  • Please change your name convention if it is possible because it is hard for me to know what your names mean.

  • Try reducing the mesh size and go back to steady-state to ensure that that works before jumping into a high cell count transient simulation.

P.S.: Are you talking about the CFD Master Class - Session 1 ? The step-by-step instruction is very good and you should be on the right track using it.

Cheers,

Jousef