Hot combustion gases flow into a nozzle at low velocity

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Reference no: EM13718028

Hot combustion gases flow into a nozzle at low velocity with an enthalpy of 1,000 kJ/kg at a mass flow rate of 1 kg/s. At the nozzle exit, the enthalpy is reduced by a factor of 2. What is the thrust experienced by the nozzle as a result of the exhaust gas momentum change?

Reference no: EM13718028

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