Fig. 1. Schematic of direct-connection supersonic combustion setup

Fig. 2. Detector signals. (a) Before ignition in combustion chamber; (b) after ignition in combustion chamber

Fig. 3. Measured velocity results. (a) Isolation section; (b) combustion outlet

Fig. 4. Measured results. (a) Gas temperature; (b) mole fraction of H₂O in gas; (c) gas pressure in isolation section; (d) gas pressure in extended section

Fig. 5. Measured results of shock wave in isolation section. (a) Gas velocity; (b) gas temperature; (c) mole fraction of H₂O in gas; (d) gas pressure

Fig. 6. Variation of gas mass flux in isolation sectionwith time