Question: This problem is related with compressible flows. 4 - A converging - diverging nozzle designed to produce a Mach 2 flow at the exit plane

This problem is related with compressible flows.
4- A converging-diverging nozzle designed to produce a Mach 2 flow at the exit plane is connected to a reservoir containing air at 3 MPa . For an ambient pressure of 96 kPa , the nozzle is underexpanded and a Prandtl-Meyer fan will be attached to the lip of the nozzle. Find the angle through which the Prandtl-Meyer expansion will turn the flow. Sketch the flow field immediately downstream of the nozzle exit plane; include the initial and final expansion fan angles.
This problem is related with compressible flows.

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