Print Email Facebook Twitter Residual strength of (0, ±45)s and (±45, 0)s carbon/epoxy laminates Title Residual strength of (0, ±45)s and (±45, 0)s carbon/epoxy laminates Author 't Hart, W.G.J. Institution National Aerospace Laboratory NLR Date 1977-11-01 Subject fatigue testsaircraft structuresresidual stresscomposite materialsstress concentrationlaminatescarhon fiher reinforced plasticsstress-strain diagramsfatigue strengthopenings To reference this document use: http://resolver.tudelft.nl/uuid:52ab8bd0-8a08-42be-a314-c1d075ee2df9 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 77115 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1977 National Aerospace Laboratory NLR Files PDF NLR_TR_77115_U.pdf 11.83 MB Close viewer /islandora/object/uuid:52ab8bd0-8a08-42be-a314-c1d075ee2df9/datastream/OBJ/view