Print Email Facebook Twitter Residual strength properties of carbon/epoxy composite material Title Residual strength properties of carbon/epoxy composite material Author 't Hart, W.G.J. Institution National Aerospace Laboratory NLR Date 1977-03-01 Abstract Fatigue tests on unidirectional Ca/ep composite material have been performed to investigate whether previous fatigue loading did influence the residual static strength. Residual strength tests were carried out on (0, ± 45)2s and (± 45)2s laminates, while for the (O, ± 45)2s laminate the influence of previous tensile fatigue loading on the residual strength was investigated. Subject composite materialscarhon fiher reinforced plasticsfracture strengthfatigue testscyclic loadsstress concentrationopeningsresidual strengthairframe materialscrack initiationcritical loadingfatigue life To reference this document use: http://resolver.tudelft.nl/uuid:453d7e49-aa4e-45b3-8bf7-9fa848094faa Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 77039 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1977 National Aerospace Laboratory NLR Files PDF NLR_TR_77039_U.pdf 13.41 MB Close viewer /islandora/object/uuid:453d7e49-aa4e-45b3-8bf7-9fa848094faa/datastream/OBJ/view