Hi all, I am interested in running the compressible flow solver (in principle just inviscid Euler) at supersonic Mach number on a sharp-leading-edge airfoil (attached shock expected). The solver seems to run just fine, but when I try to activate the shock-capturing option, the execution fails. I tried to find among the tests and examples the transonic airfoil case shown in the user-guide but I couldn't find it, plus the guide is not very clear on how to use shock-capturing. Can someone share a conditions file that has shock-capturing activated with the compressible Euler solver? Thanks in advance for any help with this. Cheers