New reliability-based optimisation scheme applied to a composite fuselage panel
New reliability-based optimisation scheme applied to a composite fuselage panel
| dc.contributor.author | Grooteman, F.P. | en_US |
| dc.date.accessioned | 2012-03-09T13:18:49Z | |
| dc.date.available | 2012-03-09T13:18:49Z | |
| dc.date.issued | 2011 | en_US |
| dc.identifier.other | NLR-TP-2011-248 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/128 | |
| dc.language.iso | en | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2011-248 | en_US |
| dc.subject.other | Composite materials | en_US |
| dc.subject.other | Aeronautics | en_US |
| dc.title | New reliability-based optimisation scheme applied to a composite fuselage panel | en_US |
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