Consider the flow through a convergent-divergent duct with an exit-to-throat area ratio of 2. The reservoir pressure
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Consider the flow through a convergent-divergent duct with an exit-to-throat area ratio of 2. The reservoir pressure is \(1 \mathrm{~atm}\), and the exit pressure is \(0.95 \mathrm{~atm}\). Calculate the Mach numbers at the throat and at the exit.
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