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Engineering, 02.03.2020 23:56 Oliviapuffinburger33

In this problem we will do a small analysis of flow with heat addition (Rayleigh flow) in a constant area duct. Let us refer to the inlet and exit sections of the constant areas duct as 1 and 2. Plot the exit Mach number (M2) as a function of the heat addition parameter for the following cases: a) Inlet Mach number is subsonic (M = 0.3)

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