The reservoir pressure and temperature for a convergent-divergent nozzle are 5atm and 520R, respectively. The flow is

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The reservoir pressure and temperature for a convergent-divergent nozzle are 5atm and 520°R, respectively. The flow is expanded isentropically to supersonic speed at the nozzle exit. If the exit-to-throat area ratio is 2.193, calculate the following properties at the exit: Me, pe, Te, pe, ue, p0, e, T0, e.

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