A seven-point bending test to determine the strength of the skin-stiffener interface in composite aircraft panels

dc.contributor.author Rijn, J.C.F.N. van en_US
dc.contributor.author Wiggenraad, J.F.M. en_US
dc.date.accessioned 2013-10-30T12:52:59Z
dc.date.available 2013-10-30T12:52:59Z
dc.date.issued 2000 en_US
dc.identifier.other NLR-TP-2000-044 en_US
dc.identifier.uri http://hdl.handle.net/10921/815
dc.language.iso en en_US
dc.publisher National Aerospace Laboratory NLR en_US
dc.relation.ispartofseries NLR Technical Publication;2000-044 en_US
dc.subject.other SM test facilities en_US
dc.subject.other Composite materials en_US
dc.title A seven-point bending test to determine the strength of the skin-stiffener interface in composite aircraft panels en_US
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