1.

The thermal efficiency of Gas turbine plant is (Where r is pressure ratio and γ is relation between specific heats).

A. \(r^{\gamma -1}\)
B. \(1-r^{\gamma -1}\)
C. \(1-(1/r)^{\gamma /(\gamma -1)}\)
D. \(1-(1/r)^{(\gamma -1)/\gamma }\)
Answer» D. \(1-(1/r)^{(\gamma -1)/\gamma }\)


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