Fatigue crack growth in highly loaded components

Simple item page
dc.contributor.authorHuls, R.A.en_US
dc.contributor.authorGrooteman, F.P.en_US
dc.contributor.authorVeul, R.P.G.en_US
dc.date.accessioned2016-01-18T10:52:01Z
dc.date.available2016-01-18T10:52:01Z
dc.date.issued2013en_US
dc.identifier.otherNLR-TP-2013-107en_US
dc.identifier.urihttp://hdl.handle.net/10921/1057
dc.language.isoenen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;2013-107en_US
dc.subject.otherStructural stabilityen_US
dc.subject.otherStructural loadsen_US
dc.titleFatigue crack growth in highly loaded componentsen_US

Files

Original bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
TP-2013-107.pdf
Size:
3.4 MB
Format:
Adobe Portable Document Format
Download

Collections

Reports