Design optimization of stiffened composite panels with buckling and damage tolerance constraints
Design optimization of stiffened composite panels with buckling and damage tolerance constraints
| dc.contributor.author | Wiggenraad, J.F.M. | en_US |
| dc.contributor.author | Arendsen, P. | en_US |
| dc.contributor.author | Silva Pereira, J.M. de | en_US |
| dc.date.accessioned | 2017-02-13T12:26:42Z | |
| dc.date.available | 2017-02-13T12:26:42Z | |
| dc.date.issued | 1998 | en_US |
| dc.identifier.other | NLR-TP-1998-024 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/1173 | |
| dc.language.iso | nl | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;1998-024 | en_US |
| dc.subject.other | Composite materials | en_US |
| dc.subject.other | Structures and materials | en_US |
| dc.title | Design optimization of stiffened composite panels with buckling and damage tolerance constraints | en_US |
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