Investigating the effect of turbine inlet temperature on the exergetic improvement potential of a small turbojet engine

dc.contributor.author	Turan, O.
dc.contributor.author	Hepbasli, A.
dc.contributor.author	Karakoc, T.H.
dc.date.accessioned	2021-01-25T20:48:48Z
dc.date.available	2021-01-25T20:48:48Z
dc.date.issued	2017
dc.identifier	10.1109/ICMAE.2017.8038660
dc.identifier.uri	https://www.scopus.com/inward/record.uri?eid=2-s2.0-85032380071&doi=10.1109%2fICMAE.2017.8038660&partnerID=40&md5=5905ec92459281eb9efb70fcab7d3570
dc.identifier.uri	https://dspace.yasar.edu.tr/xmlui/handle/20.500.12742/10054
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 combusti
dc.language.iso	English
dc.publisher	2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
dc.title	Investigating the effect of turbine inlet temperature on the exergetic improvement potential of a small turbojet engine
dc.type	Conference Paper
dc.relation.firstpage	301
dc.relation.lastpage	304
dc.description.affiliations	Faculty of Aeronautics and Astronautics, Anadolu University, Eskisehir, Turkey; Department of Energy Systems Engineering, Yasar University, Izmir, Turkey

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