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Crack tunneling and Delamination in Fiber-Metal Laminates

A specimen of Glare 3 2/1 0.3 with an initial imperfection in the metal layer, is analysed. The aluminium and fibre-reinforced prepeg layers are modeled using continuum solid like shell elements. Delamination between the metal and the fibre-epoxy layer and mode I crack in the aluminium layer are modelled in a discrete manner using interface elements.

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