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 Şöhret
Selcuk Ekici
Onder Altuntas
A. Hepbasli
Hikmet Tahir Karakoc
Journal Title
Journal ISSN
Volume Title
Publisher
Elsevier 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. © 2017 Elsevier B.V. All rights reserved.
Description
Keywords
Aircraft, Exergy, Gas Turbine Engine, Review, Thermodynamic Analysis, Aircraft, Aircraft Engines, Aircraft Propulsion, Alternative Fuels, Combustion, Combustion Chambers, Engines, Exergy, Fighter Aircraft, Gas Fuel Analysis, Gases, Reviews, Sustainable Development, Thermoanalysis, Thermodynamics, Turbine Components, Aircraft Gas Turbine Engines, Assessment Methodologies, Conventional Fuel, Environmental Science, Literature Overview, Performance Assessment, Thermal Engineering, Thermo Dynamic Analysis, Gas Turbines, Aircraft, Aircraft engines, Aircraft propulsion, Alternative fuels, Combustion, Combustion chambers, Engines, Exergy, Fighter aircraft, Gas fuel analysis, Gases, Reviews, Sustainable development, Thermoanalysis, Thermodynamics, Turbine components, Aircraft gas turbine engines, Assessment methodologies, Conventional fuel, Environmental science, Literature overview, Performance assessment, Thermal engineering, Thermo dynamic analysis, Gas turbines
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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