Question: Air flow system shown in the figure below is designed to generate supersonic flow at the exit of the C - D nozzle without shock

Air flow system shown in the figure below is designed to generate supersonic flow at the exit of the C-D nozzle without shock or expansion wave (pb=pe=1atm ). All dimensions are shown in the figure, the pipe has an average friction coefficient of f=0.005.(a) Determine the stagnation pressure in the tank need to be maintained in the tank. (b) Show the flow process on a T-s diagram. Show work please
Air flow system shown in the figure below is

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