Engine performance prediction for varied low pressure turbine vane geometry utilizing test rig data and combined computational fluid dynamic and cycle models

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dc.contributor.authorRooij, M.P.C. vanen_US
dc.contributor.authorKogenhop, O.en_US
dc.contributor.authorRademaker, E.R.en_US
dc.contributor.authorWoodason, R.en_US
dc.contributor.authorSoemarwoto, B.I.en_US
dc.date.accessioned2013-09-16T09:53:46Z
dc.date.available2013-09-16T09:53:46Z
dc.date.issued2012en_US
dc.identifier.otherNLR-TP-2012-482en_US
dc.identifier.urihttp://hdl.handle.net/10921/508
dc.language.isoenen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;2012-482en_US
dc.subject.otherGasturbine technologyen_US
dc.subject.otherTurbomachinery flowen_US
dc.titleEngine performance prediction for varied low pressure turbine vane geometry utilizing test rig data and combined computational fluid dynamic and cycle modelsen_US

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