The fifth generation fighter aircraft Eurofighter Typhoon is equipped with two EJ- 200 Jet Engines as shown in Figure below. In a non-combat operation, both jet engines propel the Eurofighter Typhoon at 300 m/s the through air at 60 kPa and 0C. For each jet engine, the inlet diameter is 2.0 m, the compressor pressure ratio is 10, and the temperature at the turbine inlet is 450C. Determine the velocity at the exit of each engine's nozzle and the total thrust produced. Assume ideal operation for all components and constant specific heat at room temperature. (You must show the process in a T-s diagram)

Euro Fighter Typhoon Air Exit Air Inlet EJ200 Air Inlet www Air Inlet Diffuser Compressor Combustion Turbine Nozzle 6 Air Exit Air Exit