Calculate the mach number (mt) and pressure

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Reference no: EM13963921

A convergent-divergent nozzle with an exit-to-throat area ration of 1.616 has exit and reservoir pressures equal to 0.947 and 1.0 atm, respectively.

Assuming isentropic flow through the nozzle, calculate the Mach number (Mt) and pressure (Pt at the throat)

Reference no: EM13963921

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