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dc.contributor.authorWanhill, R.J.H.en_US
dc.contributor.authorBarter, S.A.en_US
dc.contributor.authorHattenberg, T.en_US
dc.contributor.authorHuls, R.A.en_US
dc.contributor.authorUbels, L.C.en_US
dc.contributor.authorBos, M.J.en_US
dc.date.accessioned2012-03-12T09:55:09Z
dc.date.available2012-03-12T09:55:09Z
dc.date.issued2009en_US
dc.identifier.otherNLR-TP-2009-596en_US
dc.identifier.urihttp://hdl.handle.net/10921/260
dc.language.isoenen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;2009-596en_US
dc.subject.otherMetallic materialsen_US
dc.subject.otherStructural stabilityen_US
dc.titleFractography-assisted Observations on Fatigue Thresholds in an Aerospace Aluminium Alloyen_US


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