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Problem 13.38 - Problem 13.38[Difficulty 3 Given Air flow...

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Problem 13.38 [Difficulty: 3] Given: Air flow through a converging-diverging nozzle Find: Nozzle exit area and mass flow rate Solution: The given or available data is: R = 286.9 J/kg-K k = 1.4 p 0 = 2 MPa T 0 = 313 K p e = 200 kPa A t = 20 cm 2 Equations and Computations: Using the stagnation to exit static pressure ratio, we can find the exit Mach number: (using built-in function Isenp ( M , k ))
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