A gas turbine plant receives air at 1 bar and 290°K and compresses it to 5 bar. If the temperature of air after compression is 1000°K; find the thermal efficiency of the turbine
η=p1T2p2T1=0.69=69%.\eta=\frac{p_1T_2}{p_2T_1}=0.69=69\%.η=p2T1p1T2=0.69=69%.
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