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Gas turbine engine performance model applications using an object-oriented simulation tool

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dc.contributor.author Alexiou, A en
dc.contributor.author Mathioudakis, K en
dc.date.accessioned 2014-03-01T02:44:04Z
dc.date.available 2014-03-01T02:44:04Z
dc.date.issued 2006 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/31648
dc.relation.uri http://www.scopus.com/inward/record.url?eid=2-s2.0-33750842669&partnerID=40&md5=f8ecc23219b16d0fd6640a2a8bb0f7a5 en
dc.relation.uri http://www.ltt.mech.ntua.gr/paperfull/GT2006-90339.pdf en
dc.subject Gas turbine en
dc.subject Object-oriented en
dc.subject Performance en
dc.subject Simulation en
dc.subject.other Computer simulation en
dc.subject.other Life cycle en
dc.subject.other Mathematical models en
dc.subject.other Object oriented programming en
dc.subject.other Product design en
dc.subject.other Product development en
dc.subject.other Engine components en
dc.subject.other Engine performance en
dc.subject.other Object-oriented simulation tool en
dc.subject.other Gas turbines en
dc.title Gas turbine engine performance model applications using an object-oriented simulation tool en
heal.type conferenceItem en
heal.publicationDate 2006 en
heal.abstract Engine performance models are used throughout the life cycle of an engine from conceptual design to testing, certification and maintenance. The objective of this paper is to demonstrate the use and advantages of an engine performance model, developed using an object-oriented simulation tool, for the following applications: Building an engine model from existing engine components and running steady state and transient calculations Development and integration of a new cooled turbine component in the existing engine model Accessing the engine model from an external application Using an external legacy routine in the engine model Copyright © 2006 by ASME. en
heal.journalName Proceedings of the ASME Turbo Expo en
dc.identifier.volume 2 en
dc.identifier.spage 109 en
dc.identifier.epage 116 en


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