Comparative Performance Metric Assessment of A Military Turbojet Engine Utilizing Hydrogen And Kerosene Fuels Through Advanced Exergy Analysis Method

dc.contributor.author	Yuksel, B.
dc.contributor.author	Balli, O.
dc.contributor.author	Gunerhan, H.
dc.contributor.author	Hepbasli, A.
dc.date.accessioned	2021-01-25T19:32:38Z
dc.date.available	2021-01-25T19:32:38Z
dc.date.issued	2020
dc.identifier	10.3390/en13051205
dc.identifier.uri	https://dspace.yasar.edu.tr/xmlui/handle/20.500.12742/7311
dc.description.abstract	This study dealt with evaluating the (J85-GE-5H) military turbojet engine (TJE) in terms of exergetic and advanced exergetic analyses at Military (MIL) and Afterburner (AB) process modes by utilizing kerosene (JP-8) and hydrogen (H-2) fuels. First, exergy
dc.language.iso	English
dc.publisher	MDPI
dc.title	Comparative Performance Metric Assessment of A Military Turbojet Engine Utilizing Hydrogen And Kerosene Fuels Through Advanced Exergy Analysis Method
dc.type	Article
dc.relation.volume	13
dc.relation.issue	5
dc.description.woscategory	Energy & Fuels
dc.description.wosresearcharea	Energy & Fuels
dc.identifier.wosid	WOS:000524318700192

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