A converging-diverging nozzle is designed to operate with an exit Mach number of 2. The nozzle...

(a) The ratio of exit-to-throat area and exit area.
(b) Given the area ratio in part (a), find the range of back pressure over which the nozzle is choked. What is the critical pressure and design pressure?
Also, calculate the mass flow rate when the nozzle is choked and at design conditons.
(c) Determine the mass flow rate for a back pressure of 450 kPa and 500 kPa.
(d) Determine the mass flow rate for a back pressure of 0 kPa.
(e) Plot pressure variation along centerline of nozzle and mark all the points (back pressures) on it.
(f) Use excel sheet to plot mass variation Vs back pressures and mark all points on it.

Solutions

Expert Solution

As per guidelines, first 4 subparts are solved. Please repost the remaining question.

samet mamat answered 4 months ago

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