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Thermodynamic analysis of indirect injection diesel engines by two-zone modeling of combustion

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dc.contributor.author Kouremenos, DA en
dc.contributor.author Rakopoulos, CD en
dc.contributor.author Hountalas, D en
dc.date.accessioned 2014-03-01T01:08:11Z
dc.date.available 2014-03-01T01:08:11Z
dc.date.issued 1990 en
dc.identifier.issn 0742-4795 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/10323
dc.subject Diesel Engine en
dc.subject Thermodynamics en
dc.subject.classification Engineering, Mechanical en
dc.subject.other Combustion--Mathematical Models en
dc.subject.other Thermodynamics en
dc.subject.other Burning Model en
dc.subject.other Combustion Two Zone Model en
dc.subject.other Conservation Equations en
dc.subject.other Indirect Injection Diesel Engines en
dc.subject.other Diesel Engines en
dc.title Thermodynamic analysis of indirect injection diesel engines by two-zone modeling of combustion en
heal.type journalArticle en
heal.identifier.primary 10.1115/1.2906468 en
heal.identifier.secondary http://dx.doi.org/10.1115/1.2906468 en
heal.language English en
heal.publicationDate 1990 en
heal.abstract This work presents a thermodynamic analysis of a naturally aspirated, four-stroke, diesel engine with a swirl prechamber, under firing conditions during the open and closed part of the cycle. For calculating the heat exchange between gas and walls in both the main chamber and (swirl) prechamber, the relevant characteristic velocities and lengths are calculated by setting up a zero-dimensional energy cascade turbulence model. One-dimensional, quasi-steady, compressible flow with heat transfer inside the throat passageway connecting the two chambers is used. Combustion in both the main chamber and the swirl prechamber is attacked by proposing a two-zone combustion model, and following the movement of the spray plume inside an air solid body rotation environment in the prechamber and its later progression into the main chamber through the connecting throat. en
heal.publisher ASME-AMER SOC MECHANICAL ENG en
heal.journalName Journal of Engineering for Gas Turbines and Power en
dc.identifier.doi 10.1115/1.2906468 en
dc.identifier.isi ISI:A1990EE53000021 en
dc.identifier.volume 112 en
dc.identifier.issue 1 en
dc.identifier.spage 138 en
dc.identifier.epage 149 en


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