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Consider a supersonic nozzle with a Pitot tube mounted at the exit. The reservoir pressure and temperature are 10 atm and 500 K, respectively. The pressure measured by the Pitot tube is 0.6172 atm. The throat area is 0.3 m2.
Calculate:
a. Exit Mach number Me
b. Exit area Ae
c. Exit pressure and temperature pe and Te
d. mass flow through the nozzle

Sagot :

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