A converging-diverging nozzle has a design mach number of

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A converging-diverging nozzle has a design Mach number of 2.0 . The stagnation pressure at the nozzle inlet is 100 psia. The nozzle exhausts to a back pressure of 5 psia. Sketch the flow field downstream of the nozzle exit and determine: (a) The exit pressure of the nozzle (b) The Mach number, flow direction, and pressure immediately outside the nozzle.

Reference no: EM13627011

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