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
OpenAIRE Downloads
OpenAIRE Views
Publicly Funded
No
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
Citation
WoS Q
Scopus Q

OpenCitations Citation Count
77
Source
Progress in Aerospace Sciences
Volume
83
Issue
Start Page
57
End Page
69
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Citations
CrossRef : 28
Scopus : 80
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Mendeley Readers : 119
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