Exergy as a useful tool for the performance assessment of aircraft gas turbine engines: A key review

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Date

2016

Authors

Yasin Sohret
Selcuk Ekici
Onder Altuntas
Arif Hepbasli
T. Hikmet Karakoc

Journal Title

Journal ISSN

Volume Title

Publisher

PERGAMON-ELSEVIER SCIENCE LTD

Open Access Color

Green Open Access

No

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No
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Top 1%
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Top 10%
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Top 10%

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Abstract

It is known that aircraft gas turbine engines operate according to thermodynamic principles. Exergy is considered a very useful tool for assessing machines working on the basis of thermodynamics. In the current study exergy-based assessment methodologies are initially explained in detail. A literature overview is then presented. According to the literature overview turbofans may be described as the most investigated type of aircraft gas turbine engines. The combustion chamber is found to be the most irreversible component and the gas turbine component needs less exergetic improvement compared to all other components of an aircraft gas turbine engine. Finally the need for analyses of exergy exergo-economic exergo-environmental and exergo-sustainability for aircraft gas turbine engines is emphasized. A lack of agreement on exergy analysis paradigms and assumptions is noted by the authors. Exergy analyses of aircraft gas turbine engines fed with conventional fuel as well as alternative fuel using advanced exergy analysis methodology to understand the interaction among components are suggested to those interested in thermal engineering aerospace engineering and environmental sciences. (C) 2016 Elsevier Ltd. All rights reserved.

Description

Keywords

Exergy, Thermodynamic analysis, Aircraft, Gas turbine engine, Review, EXERGOECONOMIC ANALYSIS, TURBOPROP ENGINE, TURBOFAN ENGINE, TURBOJET ENGINE, SUSTAINABILITY INDICATORS, ENVIRONMENTAL-IMPACT, ENTROPY GENERATION, ENERGY, VEHICLE, OPTIMIZATION, Thermodynamic Analysis, Gas Turbine Engine, Exergy, Review, Aircraft

Fields of Science

0202 electrical engineering, electronic engineering, information engineering, 02 engineering and technology

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OpenCitations Citation Count
77

Source

Progress in Aerospace Sciences

Volume

83

Issue

Start Page

57

End Page

69
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Scopus : 80

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80

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Web of Science™ Citations

69

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