Homework Statement
In a jet engine, a flow of air at 1000 K, 200 kPa, and 40 m/s enters a nozzle, where the air exits at 500 m/s and 90 kPa. What is the exit temperature, inlet area, and exit area, assuming no heat loss?
Homework Equations
min = mout = m
where m = mass air flow
dE/dt cv = Qcv...