Performance Simulation of an ideal mixer-ejector turbofan engine for a supersonic business jet
Performance Simulation of an ideal mixer-ejector turbofan engine for a supersonic business jet
| dc.contributor.author | Rademaker, E.R. | en_US |
| dc.date.accessioned | 2012-03-12T09:55:07Z | |
| dc.date.available | 2012-03-12T09:55:07Z | |
| dc.date.issued | 2009 | en_US |
| dc.identifier.other | NLR-TP-2009-292 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/236 | |
| dc.language.iso | en | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2009-292 | en_US |
| dc.subject.other | Gasturbine technology | en_US |
| dc.subject.other | Air transportation | en_US |
| dc.title | Performance Simulation of an ideal mixer-ejector turbofan engine for a supersonic business jet | en_US |
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