1.

The overall thermal efficiency of an ideal gas turbine plant is (where r = Pressure ratio)

A. ɣ-1
B. - r ɣ-1
C. - (1/r) ɣ-1/ɣ
D. - (1/r) ɣ/ɣ-1
Answer» D. - (1/r) ɣ/ɣ-1


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