Print Email Facebook Twitter Residual strength of kevlar-carbon/epoxy hybrid composite materials Title Residual strength of kevlar-carbon/epoxy hybrid composite materials Author 't Hart, W.G.J. Institution National Aerospace Laboratory NLR Date 1978-01-16 Abstract Residual strength tests have been carried out on various Kevlar 49-Carbon epoxy laminate configurations consisting of a carbon/epoxy core with face sheets of Kevlar 49 fabric. The influence of fatigue loading of notched specimens on the residual strength was investigated. Subject composite materialsRotch strengthfatigue teststmixturescarbon fiber reinforced plastics To reference this document use: http://resolver.tudelft.nl/uuid:e0979fee-9889-444c-a56c-222800549a2d Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 78008 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1978 National Aerospace Laboratory NLR Files PDF NLR_TR_78008_U.pdf 10.21 MB Close viewer /islandora/object/uuid:e0979fee-9889-444c-a56c-222800549a2d/datastream/OBJ/view