engineering recuitment GATE ME 2023-24 Test Series Thermodynamics First Law of Thermodynamics Steady Flow Energy Equation
In a gas turbine, the mass of gas enters at 10 kg/s with a velocity of 60 m/s and enthalpy of 1000 kJ/kg and exits from the turbine with a velocity of 150 m/s and enthalpy of 500 kJ/kg. The heat coming out from the turbine is 25 kJ/kg. Assume for gas R = 0.285 kJ/kg K and Cp=1.004 kJ/kg and inlet conditions are 100 kPa and 27ºC. Determine power output from the turbine (in kW).
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