Question: For the same engine in Problems 9 . 1 8 - 9 . 2 0 , the pressure at the exit of the nozzle is

For the same engine in Problems 9.18-9.20, the pressure at the exit of the nozzle is p6=2,116 lb/ft^2. The pressure at the inlet to the compressor is also p3. The flow velocity entering the nozzle is V5=1,500 ft/s. Calculate the flow velocity at the nozzle exit.

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