In a gas turbine cycle, the turbine output is 600 kj/kg, the compressor work is 400kj/kg and the heat supplied is 1000 kj/kg. The thermal efficiency of this cycle is:
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Given:
Output = 600 kJ / kg
Work = 400 kJ / kg
Heat supplied = 1000 kJ / kg
To find:
Thermal efficiency.
Solution:
By formula,
Net work = Output - Work
Substituting,
We get,
600 - 400
Net work = 200 kj / kg
Thermal efficiency = Net work / Heat supplied
Substituting,
We get,
200 / 1000 * 100
Thermal efficiency = 20 %
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