Investigating the Effect of Turbine Inlet Temperature on the Exergetic Improvement Potential of a Small Turbojet Engine

dc.contributor.author Onder Turan
dc.contributor.author Arif Hepbasli
dc.contributor.author T. Hikmet Karakoc
dc.coverage.spatial 8th International Conference on Mechanical and Aerospace Engineering (ICMAE)
dc.date.accessioned 2025-10-06T16:21:13Z
dc.date.issued 2017
dc.description.abstract This paper analyzes and evaluates exergetic improvement rate (IPex) of the components of a small turbojet engine with various turbine inlet temperatures. The engine consists of an inlet starter generator a centrifugal compressor a reverse flow combustion chamber an axial-flow turbine and an exhaust nozzle. IPex analysis is performed on this turbomachinery utilizing kerosene as a fuel. Exergetic analysis is applied to the turbojet to investigate the turbine inlet temperature effects (i.e. turbine material improvement) on the IPex of each component in the engine using different turbine inlet temperatures at a constant reference environment.
dc.identifier.isbn 978-1-5386-3306-9
dc.identifier.uri https://gcris.yasar.edu.tr/handle/123456789/6759
dc.language.iso English
dc.publisher IEEE
dc.relation.ispartof 8th International Conference on Mechanical and Aerospace Engineering (ICMAE)
dc.source 2017 8TH INTERNATIONAL CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ICMAE)
dc.subject propulsion, turbomachinery, exergy, improvement potential: second law analysis, turbojet
dc.title Investigating the Effect of Turbine Inlet Temperature on the Exergetic Improvement Potential of a Small Turbojet Engine
dc.type Conference Object
dspace.entity.type Publication
gdc.coar.type text::conference output
gdc.index.type WoS
oaire.citation.endPage 304
oaire.citation.startPage 301
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relation.isOrgUnitOfPublication.latestForDiscovery ac5ddece-c76d-476d-ab30-e4d3029dee37

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