Failure criterion for the skin-stiffener interface in composite aircraft panels
Failure criterion for the skin-stiffener interface in composite aircraft panels
| dc.contributor.author | Rijn, J.C.F.N. van | en_US |
| dc.date.accessioned | 2017-02-13T12:26:44Z | |
| dc.date.available | 2017-02-13T12:26:44Z | |
| dc.date.issued | 1998 | en_US |
| dc.identifier.other | NLR-TP-1998-264 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/1206 | |
| dc.language.iso | nl | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;1998-264 | en_US |
| dc.subject.other | Composite materials | en_US |
| dc.subject.other | Structural stability | en_US |
| dc.title | Failure criterion for the skin-stiffener interface in composite aircraft panels | en_US |
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