settling chamber x = 0.0 m h = 0.94 m x = 0.5 m h = 0.57m x = 3.5 m h = 1.50 m x = 5.0 m h = 1.50 m heat exhanger - normal shock nozzle test section compressor Figure 3: Schematic of supersonic wind tunnel x = 8.0 m h = 1.50 m