A gas turbine engine operates between minimum temperature (T_{1}) and maximum temperature (T_{3}). Show that the optimum

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A gas turbine engine operates between minimum temperature \(T_{1}\) and maximum temperature \(T_{3}\). Show that the optimum pressure ratio for maximum work output is

\[r_{p}=\left(\frac{T_{3}}{T_{1}}\right)^{\frac{\kappa}{2(\kappa-1)}}\]

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Advanced Thermodynamics For Engineers

ISBN: 9780080999838

2nd Edition

Authors: D. E. Winterbone, Ali Turan

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