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dc.contributor.authorŞöhret, Yasin
dc.contributor.authorKarakoç, Tahir Hikmet
dc.date.accessioned2019-10-20T19:32:24Z
dc.date.available2019-10-20T19:32:24Z
dc.date.issued2018
dc.identifier.issn1748-8842
dc.identifier.issn1758-4213
dc.identifier.urihttps://dx.doi.org/10.1108/AEAT-03-2016-0045
dc.identifier.urihttps://hdl.handle.net/11421/18471
dc.descriptionWOS: 000427148800012en_US
dc.description.abstractPurpose It is essential to develop more environment-friendly energy systems to prevent climate change and minimize environmental impact. Within this scope, many studies are performed on performance and environmental assessments of many types of energy systems. This paper, different from previous studies, aims to prove exergy performance of a low-emission combustor of an aero-engine. Design/methodology/approach It is a well-known fact that, with respect to previous exergy analysis, highest exergy destruction occurs in the combustor component of the engine. For this reason, it is required to evaluate a low-emission aero-engine combustor thermodynamically to understand the state of the art according to the authors' best of knowledge. In this framework, combustor has been operated at numerous conditions (variable engine load) and evaluated. Findings As a conclusion of the study, the impact of emission reduction on performance improvement of the aero-engine combustors exergetically is presented. It is stated that exergy efficiency of the low-emission aero-engine combustor is found to be 64.69, 61.95 and 71.97 per cent under various operating conditions. Practical implications Results obtained in this paper may be beneficial for researchers who are interested in combustion and propulsion technology and thermal sciences. Originality/value Different from former studies, the impact of operating conditions on performance of a combustor is examined from the viewpoint of thermodynamics.en_US
dc.description.sponsorshipSuleyman Demirel University of Turkey; Anadolu University of Turkeyen_US
dc.description.sponsorshipThe authors would like to thank Suleyman Demirel and Anadolu Universities of Turkey for the provided support.en_US
dc.language.isoengen_US
dc.publisherEmerald Group Publishing LTDen_US
dc.relation.isversionof10.1108/AEAT-03-2016-0045en_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectAircraften_US
dc.subjectGas Turbineen_US
dc.subjectClean Combustoren_US
dc.subjectCombustion Chamberen_US
dc.subjectExergyen_US
dc.subjectThermodynamicsen_US
dc.titleExergy indicators of a low-emission aero-engine combustoren_US
dc.typearticleen_US
dc.relation.journalAircraft Engineering and Aerospace Technologyen_US
dc.contributor.departmentAnadolu Üniversitesi, Havacılık ve Uzay Bilimleri Fakültesien_US
dc.identifier.volume90en_US
dc.identifier.issue2en_US
dc.identifier.startpage344en_US
dc.identifier.endpage350en_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US]
dc.contributor.institutionauthorKarakoç, Tahir Hikmet


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