Modeling approach to calculate redistributions of HPT-shroud cooling channels including some turbine blade tip effects

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dc.contributor.authorRademaker, E.R.en_US
dc.contributor.authorHuls, R.A.en_US
dc.contributor.authorSoemarwoto, B.I.en_US
dc.contributor.authorGestel, R. vanen_US
dc.date.accessioned2016-01-18T10:48:46Z
dc.date.available2016-01-18T10:48:46Z
dc.date.issued2013en_US
dc.identifier.otherNLR-TP-2013-172en_US
dc.identifier.urihttp://hdl.handle.net/10921/1056
dc.language.isoenen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;2013-172en_US
dc.subject.otherGasturbine technologyen_US
dc.subject.otherTurbomachinery flowen_US
dc.titleModeling approach to calculate redistributions of HPT-shroud cooling channels including some turbine blade tip effectsen_US

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