For a nozzle with the following data \(\frac {A_e}{A_t}\) = 1.616, P0 – McqOptions

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1.	For a nozzle with the following data \(\frac {A_e}{A_t}\) = 1.616, P01 = 1 atm, Pe = 0.947 atm, what is the the Mach number at the throat of the nozzle?
A.	0.25
B.	0.50
C.	0.75
D.	0.58
Answer» C. 0.75

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