Fatigue initiation and crack growth behaviour in GLARE from the Airbus MegaLiner Barrel test
Fatigue initiation and crack growth behaviour in GLARE from the Airbus MegaLiner Barrel test
| dc.contributor.author | Wanhill, R.J.H. | en_US |
| dc.contributor.author | Hattenberg, T. | en_US |
| dc.contributor.author | Haan, P.H. de | en_US |
| dc.date.accessioned | 2012-03-14T09:52:56Z | |
| dc.date.available | 2012-03-14T09:52:56Z | |
| dc.date.issued | 2006 | en_US |
| dc.identifier.other | NLR-TP-2006-276 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/338 | |
| dc.language.iso | en | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2006-276 | en_US |
| dc.subject.other | Composite materials | en_US |
| dc.subject.other | Structural stability | en_US |
| dc.title | Fatigue initiation and crack growth behaviour in GLARE from the Airbus MegaLiner Barrel test | en_US |
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