Determine the exit pressure-temperature and area, Mechanical Engineering

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Determine the exit pressure-temperature and area

Discuss the below:

Q: a. Determine the exit pressure, temperature, and area, and the throat area.

b. Suppose that the back pressure at the nozzle exit is raised to 1.4 MPa, and that the flow remains isentropic except for a normal shock wave. Determine the exit Mach number and temperature, and the mass flow rate through the nozzle.

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Mechanical Engineering: Determine the exit pressure-temperature and area

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Mechanical Engineering: Determine the exit pressure-temperature and area

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