A jet propulsion engine has an air that enter the compressor at100 kPa and 290K. The pressure ratio across the compressor is 14and the turbine inlet temperature is 1500K. When the air leaves theturbine, it enters the nozzle and expands to 100kPa. Determine thepressure at the nozzle inlet and the velocity of the air leavingthe nozzle
Important notes: Please be neat and write legibly, it’simportant that I understand your writing and follow your thoughts.And write what tables you are using and solving every step withfully details and from which tables you got the numbers pleasesolve it clearly
