Air enters an adiabatic nozzle steadily at 330 kPa, 230 °C, and 69 m/s and leaves at 108 kPa and 200 m/s. The inlet area of the nozzle is 114 cm². Determine: (a) the mass flow rate through the nozzle (kg/s), (b) the exit temperature of the air (°C), and (c) the exit area of the nozzle (cm²). Submit your solution by multiplying (a)*(b)*(c) = _______
