Design for manufacturing of fuselage panels with curved grid stiffening
Design for manufacturing of fuselage panels with curved grid stiffening
| dc.contributor.author | Brink, W.M. van den | en_US |
| dc.contributor.author | Vankan, W.J. | en_US |
| dc.date.accessioned | 2014-09-05T13:22:23Z | |
| dc.date.available | 2014-09-05T13:22:23Z | |
| dc.date.issued | 2013 | en_US |
| dc.identifier.other | NLR-TP-2013-310 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/955 | |
| dc.language.iso | en | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2013-310 | en_US |
| dc.subject.other | Composite materials | en_US |
| dc.title | Design for manufacturing of fuselage panels with curved grid stiffening | en_US |
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