A gas turbine engine operates at temperature between 300 and (1200 mathrm{~K}). The pressure ratio is 12
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A gas turbine engine operates at temperature between 300 and \(1200 \mathrm{~K}\). The pressure ratio is 12 and the working fluid is \(\mathrm{CO}_{2}\). Assume an isentropic process,
(1) Determine the efficiency and work ratio of the cycle. Assume heat capacity ratio of \(\mathrm{CO}_{2}, \kappa_{\mathrm{CO}_{2}}=1.3\).
(2) Calculate the maximum net work. Assume \(c_{p\left(\mathrm{CO}_{2}\right)}=0.9 \mathrm{~kJ} / \mathrm{kgK}\)
\([0.436,0.556,270 \mathrm{~kJ} / \mathrm{kg}]\)
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Related Book For
Advanced Thermodynamics For Engineers
ISBN: 9780080999838
2nd Edition
Authors: D. E. Winterbone, Ali Turan
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