Isentropic ally through a convergent-divergent nozzle

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Reference no: EM13714110

Air at a stagnation pressure 700kPa flows isentropic ally through a convergent-divergent nozzle. The design pressure at the nozzle exit is 56 kPa. If the back pressure is raised gradually, thereby creating a shock in the divergent portion of the nozzle, calculate:

(a) the back pressure to locate the shock at the exit plane.

(b) the minimum back pressure so that the flow in the nozzle is totally subsonic

Reference no: EM13714110

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