Development of gas turbine performance models using a generic simulation tool

Alexiou, A; Mathioudakis, K

dc.contributor.author	Alexiou, A	en
dc.contributor.author	Mathioudakis, K	en
dc.date.accessioned	2014-03-01T02:50:03Z
dc.date.available	2014-03-01T02:50:03Z
dc.date.issued	2005	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/34881
dc.relation.uri	http://www.scopus.com/inward/record.url?eid=2-s2.0-27744468364&partnerID=40&md5=bbc71ec4dcb846786f31338ab426e00a	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	Graphical user interfaces	en
dc.subject.other	Object oriented programming	en
dc.subject.other	Performance	en
dc.subject.other	Turbofan engines	en
dc.subject.other	Engine frequency response	en
dc.subject.other	Turbofan model	en
dc.subject.other	Gas turbines	en
dc.title	Development of gas turbine performance models using a generic simulation tool	en
heal.type	conferenceItem	en
heal.identifier.secondary	GT2005-68678	en
heal.publicationDate	2005	en
heal.abstract	An approach for gas turbine engine modelling using a general purpose object-oriented simulation tool is described. A commercially available such tool that can be adapted to different fields, through the creation of reusable modelling component libraries representing parts or equipment of a physical system, is employed. Libraries are developed using an object-oriented language. The possibility for quick implementation of new models and rapid analysis of results, through the use of a graphical user interface is demonstrated. A turbofan model, developed for both steady state and transient performance simulation, is used to illustrate the advantages offered by this approach. Results are presented and compared to those produced by an industry-accepted model. The flexibility of incorporating particular features into a model is demonstrated by presenting the implementation of adaptive features and a study of engine frequency response. Copyright © 2005 by ASME.	en
heal.journalName	Proceedings of the ASME Turbo Expo	en
dc.identifier.volume	1	en
dc.identifier.spage	185	en
dc.identifier.epage	194	en