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.
A convergingdiverging nozzle designed to produce a Mach flow at the exit plane is connected to a reservoir containing air at MPa For an ambient pressure of kPa the nozzle is underexpanded and a PrandtlMeyer fan will be attached to the lip of the nozzle. Find the angle through which the PrandtlMeyer expansion will turn the flow. Sketch the flow field immediately downstream of the nozzle exit plane; include the initial and final expansion fan angles.
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