Consider the addition of an afterburner to the turbojet engine in 8-2-15 [OPB] that raises the temperature

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Consider the addition of an afterburner to the turbojet engine in 8-2-15 [OPB] that raises the temperature at the inlet of the nozzle to 1300 K. Using the IG model, determine
The velocity (V) at the nozzle exit.
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