Consider an ideal jet propulsion cycle in which air enters the compressor at 100 kPa and 20oC. The pressure leaving the compressor is 1100 kPa, and the maximum temperature in the cycle is 1200oC. Air expands in the turbine at which the turbine work (WT) is equal to the compressor work (WC). On leaving the turbine, air expands in a nozzle to 100 kPa. The process is reversible and adiabatic. Determine
The velocity of the air leaving the nozzle. Use the PG model.