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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i lost in getting someone back.

i learned that people are really two-faced and no matter how angelic someone appears they always have a devil side and that you cant trust anyone anymore no matter how dear they are to you.

if your wondering who it waz it waz mah still miss her tho

~batmans wife dun dun

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i dont know the answer but good luck

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the answer is d

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i’d like brainliest . : )

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