HEAL DSpace

Secondary air system component modelling for engine performance simulations

Αποθετήριο DSpace/Manakin

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dc.contributor.author Alexiou, A en
dc.contributor.author Mathioudakis, K en
dc.date.accessioned 2014-03-01T02:51:47Z
dc.date.available 2014-03-01T02:51:47Z
dc.date.issued 2008 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/35658
dc.relation.uri http://www.scopus.com/inward/record.url?eid=2-s2.0-69949167272&partnerID=40&md5=280ed6a95313bad29fc977e762af0ab5 en
dc.subject Labyrinth seal en
dc.subject Orifice discharge coefficient en
dc.subject Performance en
dc.subject Pre-swirl system en
dc.subject Rotating cavity en
dc.subject Secondary air system en
dc.subject.other Labyrinth seal en
dc.subject.other Orifice discharge coefficient en
dc.subject.other Performance en
dc.subject.other Pre-swirl system en
dc.subject.other Rotating cavity en
dc.subject.other Secondary air system en
dc.subject.other Machine design en
dc.subject.other Orifices en
dc.subject.other Rotation en
dc.subject.other Simulators en
dc.subject.other Seals en
dc.title Secondary air system component modelling for engine performance simulations en
heal.type conferenceItem en
heal.publicationDate 2008 en
heal.abstract This paper describes the modelling of typical secondary air system elements such as rotating orifices, seals and flow passages with heat and work transfer from the surrounding surfaces. The modelling is carried out in an object-oriented simulation environment that allows the creation of different configurations in a simple and flexible manner. This makes possible to compare the performance between different designs of individual components or complete secondary air systems as well as integrate them directly in whole engine performance models. The modelling is validated against published experimental data and computational results. An example of implementation in an engine model is also presented. Copyright © 2008 by ASME. en
heal.journalName Proceedings of the ASME Turbo Expo en
dc.identifier.volume 1 en
dc.identifier.spage 123 en
dc.identifier.epage 132 en


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