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Determine the air velocity at the exit when the inlet

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Reference no: EM13617452

The exhaust nozzle of a jet engine expands air at 300kPa and 200oC adiabatically to 100kPa. Determine the air velocity at the exit when the inlet velocity is very low (can be neglected) and the nozzle isentropic efficiency is 90%.

Reference no: EM13617452

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