Consider A Supersonic Nozzle With A Pitot Tube Mounted At The Exit The Reservoir

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.

Calculate:

a. Exit Mach number Me

b. Exit area A,

c. Exit pressure and temperature p, and T,

d. mass flow through the nozzle

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