Buckling-optimized variable stiffness laminates for a composite fuselage window section

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dc.contributor.authorBrink, W.M. van denen_US
dc.contributor.authorVankan, W.J.en_US
dc.contributor.authorMaas, R.en_US
dc.date.accessioned2014-05-12T09:40:33Z
dc.date.available2014-05-12T09:40:33Z
dc.date.issued2012en_US
dc.identifier.otherNLR-TP-2012-313en_US
dc.identifier.urihttp://hdl.handle.net/10921/932
dc.language.isoenen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;2012-313en_US
dc.subject.otherStructures and materialsen_US
dc.subject.otherComposite materialsen_US
dc.titleBuckling-optimized variable stiffness laminates for a composite fuselage window sectionen_US

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