The thermal efficiency of closed cycle gas turbine is given by (a) (1-frac{1}{r_{p}^{gamma-1}}) (b) (1-frac{1}{r_{p}^{(gamma-1) / gamma}})
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The thermal efficiency of closed cycle gas turbine is given by
(a) \(1-\frac{1}{r_{p}^{\gamma-1}}\)
(b) \(1-\frac{1}{r_{p}^{(\gamma-1) / \gamma}}\)
(c) \(1-r_{p}\)
(d) \(r_{p}-1\)
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