Modeling approach to calculate redistributions of HPT-shroud cooling channels including some turbine blade tip effects
Modeling approach to calculate redistributions of HPT-shroud cooling channels including some turbine blade tip effects
| dc.contributor.author | Rademaker, E.R. | en_US |
| dc.contributor.author | Huls, R.A. | en_US |
| dc.contributor.author | Soemarwoto, B.I. | en_US |
| dc.contributor.author | Gestel, R. van | en_US |
| dc.date.accessioned | 2016-01-18T10:48:46Z | |
| dc.date.available | 2016-01-18T10:48:46Z | |
| dc.date.issued | 2013 | en_US |
| dc.identifier.other | NLR-TP-2013-172 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/1056 | |
| dc.language.iso | en | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2013-172 | en_US |
| dc.subject.other | Gasturbine technology | en_US |
| dc.subject.other | Turbomachinery flow | en_US |
| dc.title | Modeling approach to calculate redistributions of HPT-shroud cooling channels including some turbine blade tip effects | en_US |
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