Consider supersonic Fanno flow of air with an inlet Mach
Chapter 12, Problem 105P(choose chapter or problem)
Problem 105P
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, and (c) entropy s of the fluid increase, decrease, or remain constant during this process?
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