Inlet boundary conditions

[safdarianebi]

Hi,
I have a supersonic inlet in my turbomachinery case and I have used MARKER_INLET, MARKER_RIEMANN and MARKER_GILES
with TOTAL_CONDITIONS_PT option, but in some cases however the residuals behaviour shows convergence, the final mach number for inlet boundary is not equal with what I have entered for inlet b.c. and I am confused that if there is any limitation on mach number in these boundaries?
Another matter is however some test cases use MARKER_RIEMANN boundary with STATIC_SUPERSONICINFLOW_PT (or anything like that) option, I get error that MARKER_RIEMAN boundary input is not true.

It is so confusing for me!

Thanks for your time to read this.