Buckling-optimized variable stiffness laminates for a composite fuselage window section
Buckling-optimized variable stiffness laminates for a composite fuselage window section
| dc.contributor.author | Brink, W.M. van den | en_US |
| dc.contributor.author | Vankan, W.J. | en_US |
| dc.contributor.author | Maas, R. | en_US |
| dc.date.accessioned | 2014-05-12T09:40:33Z | |
| dc.date.available | 2014-05-12T09:40:33Z | |
| dc.date.issued | 2012 | en_US |
| dc.identifier.other | NLR-TP-2012-313 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/932 | |
| dc.language.iso | en | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2012-313 | en_US |
| dc.subject.other | Structures and materials | en_US |
| dc.subject.other | Composite materials | en_US |
| dc.title | Buckling-optimized variable stiffness laminates for a composite fuselage window section | en_US |
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