Validation problem

[hosseinnegahban]

I run the subsonic NACA 0012 case in tutorials for U=51m/s (M=0.15) without any modification in runScript and I only use solveCL, but the problem is that the drag coefficient is very different from the results obtained by this website https://turbmodels.larc.nasa.gov/naca0012_val.html but the CL is fine.

[friedenhe]

Make sure you are using the same condition and mesh as the NASA website