In a gas turbine, air at a temperature of (15^{circ} mathrm{C}) and 1 bar pressure enters the
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In a gas turbine, air at a temperature of \(15^{\circ} \mathrm{C}\) and 1 bar pressure enters the compressor, where it is compressed to 5 bar. Air enters the turbine at a temperature of \(815^{\circ} \mathrm{C}\) and expands to original pressure of 1 bar. Calculate the ratio of turbine work to compressor work and thermal efficiency.
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Somshukla Chakraborty
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