Using EES (or other) software, determine the shape of a
Chapter 17, Problem 17149(choose chapter or problem)
Using EES (or other) software, determine the shape of a convergingdiverging nozzle for air for a mass flow rate of 3 kg/s and inlet stagnation conditions of 1400 kPa and 2008C. Approximate the flow as isentropic. Repeat the calculations for 50-kPa increments of pressure drop to an exit pressure of 100 kPa. Plot the nozzle to scale. Also, calculate and plot the Mach number along the nozzle.
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