Entropy 2005, 7(3), 172-187; doi:10.3390/e7030172
Article

Exergy Analysis and Second Law Efficiency of a Regenerative Brayton Cycle with Isothermal Heat Addition

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Received: 6 June 2005; Accepted: 3 July 2005 / Published: 5 July 2005
This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
Abstract: The effect of two heat additions, rather than one, in a gas turbine engine is analyzed from the second law of thermodynamics point of view. A regenerative Brayton cycle model is used for this study, and compared with other models of Brayton cycle. All fluid friction losses in the compressor and turbine are quantified by an isentropic efficiency term. The effect of pressure ratio, turbine inlet temperature, ambient temperature, altitude, and altitude with variable ambient temperature on irreversibility "exergy destroyed" and second law efficiency was investigated and compared for all models. The results are given graphically with the appropriate discussion and conclusion.
Keywords: modified Brayton cycle; exergy analysis; isothermal heat addition; second law efficiency
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MDPI and ACS Style

Jubeh, N.M. Exergy Analysis and Second Law Efficiency of a Regenerative Brayton Cycle with Isothermal Heat Addition. Entropy 2005, 7, 172-187.

AMA Style

Jubeh NM. Exergy Analysis and Second Law Efficiency of a Regenerative Brayton Cycle with Isothermal Heat Addition. Entropy. 2005; 7(3):172-187.

Chicago/Turabian Style

Jubeh, Naser M. 2005. "Exergy Analysis and Second Law Efficiency of a Regenerative Brayton Cycle with Isothermal Heat Addition." Entropy 7, no. 3: 172-187.

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