Fatigue crack initiation in aerospace aluminium alloys, components and structures

Simple item page
dc.contributor.authorWanhill, R.J.H.en_US
dc.date.accessioned2012-03-14T09:53:01Z
dc.date.available2012-03-14T09:53:01Z
dc.date.issued2006en_US
dc.identifier.otherNLR-TP-2006-751en_US
dc.identifier.urihttp://hdl.handle.net/10921/395
dc.language.isoenen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;2006-751en_US
dc.subject.otherMetallic materialsen_US
dc.subject.otherStructural stabilityen_US
dc.titleFatigue crack initiation in aerospace aluminium alloys, components and structuresen_US

Files

Original bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
TP-2006-751.pdf
Size:
3.18 MB
Format:
Adobe Portable Document Format
Download

Collections

Reports