Development of an improved model for predicting fatigue crack growth in aluminium alloy helicopter airframe components

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dc.contributor.authorBos, M.J.en_US
dc.date.accessioned2012-03-22T11:03:16Z
dc.date.available2012-03-22T11:03:16Z
dc.date.issued2007en_US
dc.identifier.otherNLR-TP-2007-406en_US
dc.identifier.urihttp://hdl.handle.net/10921/414
dc.language.isoenen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;2007-406en_US
dc.subject.otherHelicoptersen_US
dc.subject.otherStructural stabilityen_US
dc.titleDevelopment of an improved model for predicting fatigue crack growth in aluminium alloy helicopter airframe componentsen_US

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