New reliability-based optimisation scheme applied to a composite fuselage panel

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dc.contributor.authorGrooteman, F.P.en_US
dc.date.accessioned2012-03-09T13:18:49Z
dc.date.available2012-03-09T13:18:49Z
dc.date.issued2011en_US
dc.identifier.otherNLR-TP-2011-248en_US
dc.identifier.urihttp://hdl.handle.net/10921/128
dc.language.isoenen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;2011-248en_US
dc.subject.otherComposite materialsen_US
dc.subject.otherAeronauticsen_US
dc.titleNew reliability-based optimisation scheme applied to a composite fuselage panelen_US

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