Dear all, I'm trying to run the test case: Inviscid transonic flow around NACA0012, from the previous 3rd High-Order Workshop (you can find a description below):
https://www.grc.nasa.gov/hiocfd/wp-content/uploads/sites/22/case_c1.2.pdf I've run the case on a coarse mesh of 2240 cells, order p3, and the parameters for the artificial viscosity method specified in the "User Guide" section of your website: [solver-artificial-viscosity] max-artvisc = 0.01 s0 = 0.01 kappa = 5.0 I obtain indistinguishable results from those without the artificial viscosity, so I guess I need to augment the max-artvisc value in order to get a higher smoothing of the shock. Could you please let me know, first, if you have run this test case or another similar, and second, which values for the parameters above to use? Also, for a more general test case, Which procedure do you use to estimate the correct value of the parameters above? I guess it's at the end a process of trial and error, but Would you know how to do a first quick estimation? Thanks a lot for your help. Best regards, Antonio -- You received this message because you are subscribed to the Google Groups "PyFR Mailing List" group. To unsubscribe from this group and stop receiving emails from it, send an email to [email protected]. To post to this group, send an email to [email protected]. Visit this group at https://groups.google.com/group/pyfrmailinglist. For more options, visit https://groups.google.com/d/optout.
