Fatigue and flaw tolerance design approach for helicopter airframe

dc.contributor.author	Galletti, N.
dc.contributor.author	Monticelli, P.
dc.contributor.author	Tirelli, M.
dc.date.accessioned	2016-07-01T14:38:16Z
dc.date.available	2016-07-01T14:38:16Z
dc.date.issued	2006
dc.identifier.other	SM03
dc.identifier.uri	http://hdl.handle.net/20.500.11881/1140
dc.language.iso	en
dc.subject.other	Structures and Materials
dc.title	Fatigue and flaw tolerance design approach for helicopter airframe

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