Shock wave laminar boundary layer interaction (SWBLI) over a double wedge at Mach 7.14 and 7.11 were simulated using the commercial flow solver GASPex. An inviscid simulation was performed at Mach 7.14 for validation. Results for the region downstream of the first shock wave show less than one percent error in comparison with oblique shock wave theory. Laminar perfect gas simulations were performed for stagnation enthalpies of 2 MJ/kg and 8 MJ/kg. The computed heat transfer distribution agrees closely with the experiment upstream of the shock wave laminar boundary layer interaction; however, significant differences are evident in the region of the interaction. In particular, the time-accurate simulations indicate a significantly longer physical time to achieve steady state than observed in the experiment.
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