Consider supersonic Fanno flow of air with an inlet Mach number of 1.8. If the Mach number

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Consider supersonic Fanno flow of air with an inlet Mach number of 1.8. If the Mach number decreases to 1.2 at the duct exit as a result of friction, does the 

(a) Stagnation temperature T0

(b) Stagnation pressure P0, 

(c) Entropy s of the fluid increase, decrease, or remain constant during this process?

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