The thermal efficiency of an ideal gas turbine plant is given by (where r = Pressure ratio)
rγ - 1
1 - rγ - 1
\(1 - (\frac { 1 } { r } )^{y/y-1}\)
\(1 - (\frac { 1 } { r })^Y-1/Y\)
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Answer : Option D
Explanation :
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