I was trying to do an aerodynamic analysis of a wing with the code saturne gui, but the problem is that, so far I was not able to extract the lift and drag coefficients of the wing. Not evene in ParaVis. I've also tryed to search for something similar in forus but was not successful.
If someone as some advice, I would be trully thankful.
I've also attached my setup file from code satune gui.
Thanks in advance
