Add V&V case, Mach 5 Shock-Wave Boundary-Layer Interaction#1651
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Although marked as WIP I guess this is safe to approve ;) and of course here as well thanks for this vandv effort 💐 (of course if you plan to add more I'll take another look 👍 )
I really like your cfg "sections" ... very well made (I usually like the little header with author, date, etc. but I also see why that is not really necessary)
pcarruscag
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Thank you @aeroamit, the intersection of supersonic inlet with the bottom wall was causing problems, I extended the inlet region 10mm and used a slip wall for the extension, the small disturbance is also visible in other numerical results in the NPARC website.
I have used the experimental data for the V&V page su2code/su2code.github.io#77

su2code/su2code.github.io#77