Failure mode estimation at highly loaded thick composite lugs representing rotary wing UAS blade root

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dc.contributor.authorTursun, G.
dc.contributor.authorMaradit, B.P.
dc.contributor.authorTaskinoglu, E.
dc.date.accessioned2016-07-01T12:58:53Z
dc.date.available2016-07-01T12:58:53Z
dc.date.issued2011
dc.identifier.otherERF 2011_198
dc.identifier.urihttp://hdl.handle.net/20.500.11881/850
dc.language.isoen
dc.titleFailure mode estimation at highly loaded thick composite lugs representing rotary wing UAS blade root

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