How can I specify the supersonic inlet profile?

[TAOSHANCONG]

When I simulate shock wave turbulent boundary layer interaction using ddes, the turbulent boundary layer profile is expected to be prescribed at the inlet to reduce the expensive computational cost. Unfortunately, SPECIFIED_INLET_PROFILE is invalid for the MARKER_SUPERSONIC_INLET. Is there a feasible tutorial for me to revise the source code of the supersonic inlet, which has been realized by Haryl Ngoh and Jonathan Poggie (https://doi.org/10.2514/1.J061102)? Or How can I specify the Mach number、static pressure and static temperature at the inlet in a compressible flow?

[pcarruscag]

We have this feature, see if there is info the PR that can help.
#2327

[TAOSHANCONG]

I am grateful for your valuable comment, I will test it and respond later.

[TAOSHANCONG]

Thanks for your help, it is feasible for me.