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A 3D finite element model using cohesive elements and continuum (bulk) material damage models was developed to examine the progressive damage and failure behaviour of Glare® Fibre Metal Laminate (FML) specimens subjected to in-plane compressive loading. The specimens contained internal ‘splice’ and ‘doubler’ features and were either pristine or contained simulated manufacturing defects in the form...
The progressive damage and fracture behaviour of Glare® fibre-metal laminates (FMLs) was investigated experimentally for the buckling and postbuckling regimes of laminates containing internal ‘splice’ and ‘doubler’ joints. Specimens were either ‘pristine’ or contained artificial delaminations in the form of strips of release film to represent manufacturing defects. Each was tested under in-plane compression...
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