Numerical data of Cp distribution
 

I'm a new user of su2

I run the Naca0012 compressible flow test case (tutorial: Epistemic Uncertainty Quantification of RANS predictions of NACA 0012 airfoil) from the command prompt (ExecSequential directory), writing

SU2_CFD turb_NACA0012_uq.cfg

I would like to get the numerical data of Cp over the airfoil's surface with the points where it's computed.

Check out surface_flow.csv or surface_flow.dat files (X vs Cp is 2nd vs 5th column I think, just open and have a look) .