(Solution) - A nozzle is designed assuming reversible adiabatic flow with an -(2025 Original AI-Free Solution)

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A nozzle is designed assuming reversible adiabatic flow with an exit Mach number of2.6 while flowing air with a stagnation pressure and temperature of 2 MPa and 150°C, respectively. The mass flow rate is 5 kg/s, and k may be assumed to be 1.40 and constant. Determine the exit pressure, temperature, exit area, and the throat area.