4- The air mass flow rate through the isentropic nozzle shown in fig. 2 is 5...

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4- The air mass flow rate through the isentropic nozzle shown in fig. 2 is 5 kg/s. Air conditions at section i are M=0.3, A=200 cm and P=300 kPa. A normal shock wave exists at section S where the area is 120 cm. Determine Po (a) the reservoir stagnation conditions (b) the pressure and temperature just To upstream and downstream the shock wave. 4- The air mass flow rate through the isentropic nozzle shown in fig. 2 is 5 kg/s. Air conditions at section i are M=0.3, A=200 cm and P=300 kPa. A normal shock wave exists at section S where the area is 120 cm. Determine Po (a) the reservoir stagnation conditions (b) the pressure and temperature just To upstream and downstream the shock wave.

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