Wisnom, MRMRWisnomCzél, GGCzélSwolfs, YYSwolfsJalalvand, MMJalalvandGorbatikh, LLGorbatikhVerpoest, IIVerpoest2016-07-112016-04-262016-07-112016-04-26Composites Part A: Applied Science and Manufacturing, 2016, 88, pp.131-1391359-835Xhttp://hdl.handle.net/10044/1/34576Experimental results are presented which allow the hybrid effect to be evaluated accurately for thin ply carbon/epoxy–glass/epoxy interlayer hybrid composites. It is shown that there is an enhancement in strain at failure of up to 20% for very thin plies, but no significant effect for thicker plies. Hybrid specimens with thick carbon plies can therefore be used to measure the reference carbon/epoxy failure strain. The latter is significantly higher than the strain from all-carbon specimens in which there is an effect due to stress concentrations at the load introduction. Models are presented which illustrate the mechanisms responsible for the hybrid effect due to the constraint on failure at both the fibre and ply level. These results give a good understanding of how variability in the carbon fibre strengths can translate into hybrid effects in composite laminates.© 2016 The Authors. Published by Elsevier Ltd. This is an open access article under the CC BY license (http:// creativecommons.org/licenses/by/4.0/).Materials0912 Materials Engineering0913 Mechanical Engineering0901 Aerospace EngineeringJournal Articlehttps://www.dx.doi.org/10.1016/j.compositesa.2016.04.014