Development of an improved model for predicting fatigue crack growth in aluminium alloy helicopter airframe components
Development of an improved model for predicting fatigue crack growth in aluminium alloy helicopter airframe components
| dc.contributor.author | Bos, M.J. | en_US |
| dc.date.accessioned | 2012-03-22T11:03:16Z | |
| dc.date.available | 2012-03-22T11:03:16Z | |
| dc.date.issued | 2007 | en_US |
| dc.identifier.other | NLR-TP-2007-406 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/414 | |
| dc.language.iso | en | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2007-406 | en_US |
| dc.subject.other | Helicopters | en_US |
| dc.subject.other | Structural stability | en_US |
| dc.title | Development of an improved model for predicting fatigue crack growth in aluminium alloy helicopter airframe components | en_US |
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