Question: The thrust developed by the engine of a Boeing 777 is about 380 kN. Assuming choked flow in the nozzle determine the mass flow rate

The thrust developed by the engine of a Boeing 777 is about 380 kN. Assuming choked flow in the nozzle determine the mass flow rate of air through the nozzle. Take the ambient conditions to be 265 K and 85 kPa.

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