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 | A. Hepbasli | |
| dc.contributor.author | Hikmet Tahir Karakoc | |
| dc.contributor.author | Turan, Onder | |
| dc.contributor.author | Hepbasli, Arif | |
| dc.contributor.author | Karakoc, T. Hikmet | |
| dc.date.accessioned | 2025-10-06T17:51:50Z | |
| 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. © 2017 Elsevier B.V. All rights reserved. | |
| dc.identifier.doi | 10.1109/ICMAE.2017.8038660 | |
| dc.identifier.isbn | 9781538633052 | |
| dc.identifier.isbn | 9781538633069 | |
| dc.identifier.scopus | 2-s2.0-85032380071 | |
| dc.identifier.uri | https://www.scopus.com/inward/record.uri?eid=2-s2.0-85032380071&doi=10.1109%2FICMAE.2017.8038660&partnerID=40&md5=a7ce9ae2738921da0955f4a4eb001986 | |
| dc.identifier.uri | https://gcris.yasar.edu.tr/handle/123456789/9650 | |
| dc.identifier.uri | https://doi.org/10.1109/ICMAE.2017.8038660 | |
| dc.language.iso | English | |
| dc.publisher | Institute of Electrical and Electronics Engineers Inc. | |
| dc.relation.ispartof | 8th International Conference on Mechanical and Aerospace Engineering ICMAE 2017 | |
| dc.rights | info:eu-repo/semantics/closedAccess | |
| dc.subject | Exergy, Improvement Potential, Propulsion, Second Law Analysis, Turbojet, Turbomachinery, Ac Generator Motors, Aerospace Engineering, Axial Flow Turbomachinery, Axial-flow Compressors, Centrifugal Compressors, Combustion Chambers, Engines, Exergy, Propulsion, Reverse Combustion, Turbine Components, Turbines, Turbomachinery, Axial Flow Turbines, Improvement Potential, Reference Environments, Second Law Analysis, Small Turbojet Engine, Starter Generators, Turbine Inlet Temperature, Turbojet, Turbojet Engines | |
| dc.subject | AC generator motors, Aerospace engineering, Axial flow turbomachinery, Axial-flow compressors, Centrifugal compressors, Combustion chambers, Engines, Exergy, Propulsion, Reverse combustion, Turbine components, Turbines, Turbomachinery, Axial flow turbines, improvement potential, Reference environments, Second law analysis, Small turbojet engine, Starter generators, Turbine inlet temperature, turbojet, Turbojet engines | |
| dc.subject | Turbomachinery | |
| dc.subject | Exergy | |
| dc.subject | Improvement Potential | |
| dc.subject | Second Law Analysis | |
| dc.subject | Propulsion | |
| dc.subject | Turbojet | |
| dc.subject | Improvement Potential: Second Law Analysis | |
| 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.author.id | Karakoc, Tahir Hikmet/0000-0001-8182-8667 | |
| gdc.author.scopusid | 54394470800 | |
| gdc.author.scopusid | 55131010100 | |
| gdc.author.scopusid | 22979722100 | |
| gdc.author.wosid | Karakoc, Tahir Hikmet/AHC-1904-2022 | |
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| gdc.description.department | ||
| gdc.description.departmenttemp | [Turan, Onder] Anadolu Univ, Fac Aeronaut & Astronaut, Eskisehir, Turkey; [Hepbasli, Arif; Karakoc, T. Hikmet] Yasar Univ, Dept Energy Syst Engn, Izmir, Turkey | |
| gdc.description.endpage | 304 | |
| gdc.description.publicationcategory | Konferans Öğesi - Uluslararası - Kurum Öğretim Elemanı | |
| gdc.description.startpage | 301 | |
| gdc.description.woscitationindex | Conference Proceedings Citation Index - Science | |
| gdc.identifier.openalex | W2754148124 | |
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| gdc.oaire.influence | 2.4486575E-9 | |
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| gdc.oaire.keywords | Turbomachinery | |
| gdc.oaire.keywords | Improvement Potential: Second Law Analysis | |
| gdc.oaire.keywords | Improvement Potential | |
| gdc.oaire.keywords | Second Law Analysis | |
| gdc.oaire.keywords | Turbojet | |
| gdc.oaire.keywords | Propulsion | |
| gdc.oaire.keywords | Exergy | |
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| gdc.oaire.sciencefields | 0203 mechanical engineering | |
| gdc.oaire.sciencefields | 02 engineering and technology | |
| gdc.oaire.sciencefields | 01 natural sciences | |
| gdc.oaire.sciencefields | 0104 chemical sciences | |
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| gdc.virtual.author | Hepbaşli, Arif | |
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| oaire.citation.endPage | 304 | |
| oaire.citation.startPage | 301 | |
| person.identifier.scopus-author-id | Turan- Onder (54394470800), Hepbasli- A. (55131010100), Karakoc- Hikmet Tahir (22979722100) | |
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