Question: A gas at a specified stagnation temperature and pressure is accelerated to Ma = 2 in a converging-diverging nozzle and to Ma = 3 in

A gas at a specified stagnation temperature and pressure is accelerated to Ma = 2 in a converging-diverging nozzle and to Ma = 3 in another nozzle. What can you say about the pressures at the throats of these two nozzles?

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