GARTEUR (AD) AG-26: Navier-Stokes computations of 3D transonic flow for a wing/fuselage configuration
GARTEUR (AD) AG-26: Navier-Stokes computations of 3D transonic flow for a wing/fuselage configuration
| dc.contributor.author | Brandsma, F.J. | en_US |
| dc.date.accessioned | 2013-10-23T08:18:38Z | |
| dc.date.available | 2013-10-23T08:18:38Z | |
| dc.date.issued | 2003 | en_US |
| dc.identifier.other | NLR-TP-2003-191 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/616 | |
| dc.language.iso | nl | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2003-191 | en_US |
| dc.subject.other | Computational fluid dynamics | en_US |
| dc.subject.other | Aeronautics | en_US |
| dc.title | GARTEUR (AD) AG-26: Navier-Stokes computations of 3D transonic flow for a wing/fuselage configuration | en_US |
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