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Simple thermodynamics of jet engines

dc.contributor.authorPatricio, Pedro
dc.contributor.authorTavares, Jose
dc.date.accessioned2011-11-28T13:09:37Z
dc.date.available2011-11-28T13:09:37Z
dc.date.issued2010-08
dc.description.abstractWe use the first and second laws of thermodynamics to analyze the behavior of an ideal jet engine. Simple analytical expressions for the thermal efficiency, the overall efficiency, and the reduced thrust are derived. We show that the thermal efficiency depends only on the compression ratio r and on the velocity of the aircraft. The other two performance measures depend also on the ratio of the temperature at the turbine to the inlet temperature in the engine, T-3/T-i. An analysis of these expressions shows that it is not possible to choose an optimal set of values of r and T-3/T-i that maximize both the overall efficiency and thrust. We study how irreversibilities in the compressor and the turbine decrease the overall efficiency of jet engines and show that this effect is more pronounced for smaller T-3/T-i.por
dc.identifier.citationPatrício P, Tavares J M. Simple thermodynamics of jet engines. American Journal of Physics. 2010; 78 (8): 809-814.por
dc.identifier.issn002-9505
dc.identifier.urihttp://hdl.handle.net/10400.21/672
dc.language.isoengpor
dc.peerreviewedyespor
dc.publisherAmer Assoc Physics Teachers Amer Inst Physicspor
dc.relation.ispartofseries8;
dc.titleSimple thermodynamics of jet enginespor
dc.typejournal article
dspace.entity.typePublication
oaire.citation.conferencePlaceMelvillepor
oaire.citation.endPage914por
oaire.citation.issue78por
oaire.citation.startPage809por
oaire.citation.titleAmerican Journal of Physicspor
person.familyNamePatricio
person.familyNameTavares
person.givenNamePedro
person.givenNameJose
person.identifier.ciencia-idC616-BA77-E9C9
person.identifier.ciencia-id371D-51C6-975C
person.identifier.orcid0000-0002-9050-9956
person.identifier.orcid0000-0002-1509-9707
person.identifier.ridA-2750-2009
person.identifier.ridA-2891-2009
person.identifier.scopus-author-id35621140500
rcaap.rightsrestrictedAccesspor
rcaap.typearticlepor
relation.isAuthorOfPublication11a2a1d5-8165-475a-8a54-e32bd8e8ce4e
relation.isAuthorOfPublication21fb8ec6-5b23-4df8-ba97-32256495d24d
relation.isAuthorOfPublication.latestForDiscovery11a2a1d5-8165-475a-8a54-e32bd8e8ce4e

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