Scaling of compressor and turbine maps on basis of equal flow Mach numbers and static flow parameters
Scaling of compressor and turbine maps on basis of equal flow Mach numbers and static flow parameters
| dc.contributor.author | Rademaker, E.R. | en_US |
| dc.date.accessioned | 2014-09-22T13:24:27Z | |
| dc.date.available | 2014-09-22T13:24:27Z | |
| dc.date.issued | 2012 | en_US |
| dc.identifier.other | NLR-TP-2012-257 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/961 | |
| dc.language.iso | en | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2012-257 | en_US |
| dc.subject.other | Gasturbine technology | en_US |
| dc.subject.other | Turbomachinery flow | en_US |
| dc.title | Scaling of compressor and turbine maps on basis of equal flow Mach numbers and static flow parameters | en_US |
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