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

dc.contributor.author Rooij, M.P.C. van en_US
dc.contributor.author Kogenhop, O. en_US
dc.contributor.author Rademaker, E.R. en_US
dc.contributor.author Woodason, R. en_US
dc.contributor.author Soemarwoto, B.I. en_US
dc.date.accessioned 2013-09-16T09:53:46Z
dc.date.available 2013-09-16T09:53:46Z
dc.date.issued 2012 en_US
dc.identifier.other NLR-TP-2012-482 en_US
dc.identifier.uri http://hdl.handle.net/10921/508
dc.language.iso en en_US
dc.publisher National Aerospace Laboratory NLR en_US
dc.relation.ispartofseries NLR Technical Publication;2012-482 en_US
dc.subject.other Gasturbine technology en_US
dc.subject.other Turbomachinery flow en_US
dc.title Engine performance prediction for varied low pressure turbine vane geometry utilizing test rig data and combined computational fluid dynamic and cycle models en_US
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