Aspects of Gas Turbine Thermal Efficiency

dc.contributor.author	Langston, Lee S.
dc.date.accessioned	2022-02-04T22:15:07Z
dc.date.available	2022-02-04T22:15:07Z
dc.date.copyright	9/1/2020 12:00:00 AM
dc.date.issued	2020
dc.identifier.issn	0025-6501
dc.identifier.other	me-2020-sep4.pdf
dc.identifier.uri	http://yetl.yabesh.ir/yetl1/handle/yetl/4275189
dc.description.abstract	In the family of heat engines, the gas turbine is unique in that it is used to produce two different kinds of useful power. By converting combusted fuel heat into work, a gas turbine engine can produce external shaft power (e.g., to drive a connected electric generator) or jet power (e.g., as a jet engine, to produce thrust forces to propel an aircraft). This means that the gas turbine’s thermodynamic figure of merit, thermal efficiency, is multifaceted, and calls for a nuanced examination.
dc.publisher	The American Society of Mechanical Engineers (ASME)
dc.title	Aspects of Gas Turbine Thermal Efficiency
dc.type	Journal Paper
dc.journal.volume	142
dc.journal.issue	9
dc.journal.title	Mechanical Engineering
dc.identifier.doi	10.1115/1.2020-SEP4
dc.journal.fristpage	54
dc.journal.lastpage	55
dc.page	2
dc.tree	Mechanical Engineering:;2020:;volume( 142 ):;issue: 009
dc.contenttype	Fulltext