The supersonic wind tunnel facility SBR-50 at the University of Notre Dame was built in 2015 for experimental research related to shock wave (SW) interactions with obstacles and boundary layers (BL) as well combustion a plasma-based flow control. Currently, provides following range parameters test section area nozzle exit 76.2 × mm: Mach number M=2 4, total pressure p0= 1–4 bar, stagnation temp...