Print Email Facebook Twitter Residual strenght and fatigue investigation on aramid-carbon/exposy laminates Title Residual strenght and fatigue investigation on aramid-carbon/exposy laminates Author 't Hart, W.G. Institution National Aerospace Laboratory NLR Date 1979-04-30 Abstract Residual strength tests have been performed on carbon/epoxy laminates with face sheets of aramid fabric. The specimens used were 40 mm wide and provided with central circular holes. Constant amplitude fatigue tests at a stress ratio of R = 0.1 have been carried out on notched and unnotched materials. To reference this document use: http://resolver.tudelft.nl/uuid:1471fa2c-e28e-4cce-9db9-8cd6e88544bd Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 80039 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1980 National Aerospace Laboratory NLR Files PDF NLR_TR_80039_U.pdf 8.37 MB Close viewer /islandora/object/uuid:1471fa2c-e28e-4cce-9db9-8cd6e88544bd/datastream/OBJ/view