A seven-point bending test to determine the strength of the skin-stiffener interface in composite aircraft panels
A seven-point bending test to determine the strength of the skin-stiffener interface in composite aircraft panels
| dc.contributor.author | Rijn, J.C.F.N. van | en_US |
| dc.contributor.author | Wiggenraad, J.F.M. | en_US |
| dc.date.accessioned | 2013-10-30T12:52:59Z | |
| dc.date.available | 2013-10-30T12:52:59Z | |
| dc.date.issued | 2000 | en_US |
| dc.identifier.other | NLR-TP-2000-044 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/815 | |
| dc.language.iso | en | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2000-044 | en_US |
| dc.subject.other | SM test facilities | en_US |
| dc.subject.other | Composite materials | en_US |
| dc.title | A seven-point bending test to determine the strength of the skin-stiffener interface in composite aircraft panels | en_US |
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