Accurate computation of drag for a wing/body configuration using multi-block, structured-grid CFD technology
Accurate computation of drag for a wing/body configuration using multi-block, structured-grid CFD technology
| dc.contributor.author | Boelens, O.J. | en_US |
| dc.contributor.author | Laban, M. | en_US |
| dc.contributor.author | Beek, C.M. van | en_US |
| dc.contributor.author | Leeden, R. van der | en_US |
| dc.date.accessioned | 2013-10-23T10:13:48Z | |
| dc.date.available | 2013-10-23T10:13:48Z | |
| dc.date.issued | 2001 | en_US |
| dc.identifier.other | NLR-TP-2001-321 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/769 | |
| dc.language.iso | nl | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2001-321 | en_US |
| dc.subject.other | Computational fluid dynamics | en_US |
| dc.subject.other | Flight mechanics / flight control | en_US |
| dc.title | Accurate computation of drag for a wing/body configuration using multi-block, structured-grid CFD technology | en_US |
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