Short and long range mission analysis for a Geared Turbofan with Active Core Technologies

Alexiou, A; Aretakis, N; Roumeliotis, I; Mathioudakis, K

dc.contributor.author	Alexiou, A	en
dc.contributor.author	Aretakis, N	en
dc.contributor.author	Roumeliotis, I	en
dc.contributor.author	Mathioudakis, K	en
dc.date.accessioned	2014-03-01T02:52:45Z
dc.date.available	2014-03-01T02:52:45Z
dc.date.issued	2010	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/36042
dc.relation.uri	http://www.scopus.com/inward/record.url?eid=2-s2.0-82055165690&partnerID=40&md5=d00bda4fb5c59046ce20faaa8e835ba5	en
dc.subject	Active control	en
dc.subject	Geared turbofan	en
dc.subject	Mission analysis	en
dc.subject.other	Active control	en
dc.subject.other	Aero-engine	en
dc.subject.other	Aircraft applications	en
dc.subject.other	Core technology	en
dc.subject.other	Engine performance	en
dc.subject.other	European program	en
dc.subject.other	Geared turbofan	en
dc.subject.other	Long range	en
dc.subject.other	Manufacturer specifications	en
dc.subject.other	Mission analysis	en
dc.subject.other	Noise levels	en
dc.subject.other	Performance Model	en
dc.subject.other	Service engine	en
dc.subject.other	Aircraft models	en
dc.subject.other	Engines	en
dc.subject.other	Environmental impact	en
dc.subject.other	Machine design	en
dc.subject.other	Marine applications	en
dc.subject.other	Program diagnostics	en
dc.subject.other	Marine engines	en
dc.title	Short and long range mission analysis for a Geared Turbofan with Active Core Technologies	en
heal.type	conferenceItem	en
heal.publicationDate	2010	en
heal.abstract	A novel engine concept, for reducing the environmental impact of gas turbines, is the Geared Turbofan with Active Core technologies (GTAC), investigated in the context of the European program NEWAC (New Aero Engine Core Concepts). Two performance models of this engine are created for short and long range aircraft applications and matched to manufacturer specifications. The engine performance data are used in a mission analysis module simulating typical aircraft applications. Compared to missions using Year 2000 in service engines, the results show a significant reduction in fuel consumption and noise levels. A significant reduction in NOx emissions requires the application of new technology combustor designs as developed e.g. in NEWAC. Copyright © 2010 by ASME.	en
heal.journalName	Proceedings of the ASME Turbo Expo	en
dc.identifier.volume	3	en
dc.identifier.spage	643	en
dc.identifier.epage	651	en