Consider a supersonic nozzle with a Pitot tube mounted at the exit. The
reservoir pressure and temperature are I0 atm and 500 K, respectively. The
pressure measured by the Pitot tube is 0.6172 atm. The throat area is 0.3 m2.
a. Exit Mach number Me
b. Exit area A,
c. Exit pressure and temperature p, and T,
d. mass flow through the nozzle