Failure mechanism under tensile loads in CFRP 0-90º cross-ply laminates containing voids

The failure mechanism of a voided CFRP 0-90° cross-ply laminate under tensile loads applied in one direction was studied in this Final Degree Project. For this purpose, voided coupons were manufactured for being tested and a FEA was done. In both investigations, voids were placed in 90º and 0º direction, in order to understand the void location influence. On the one hand, the behaviour of the voided laminates was investigated through a FEM in order to preview the stress distribution within the material. On the other hand, voided specimens where manufactured by applying blowing agent in between the inner layers. These specimens were tested by a quasi-static step wise tensile test where data showing its real behaviour was collected. Specimens were X-rayed after each step of the test in order to investigate the failure mechanism of the composite. Data from the test was studied so that relations such as strength of the laminates, crack density per stress, void length per first crack at the void and void area per first crack at the specimen could be characterized

Estudio de la adherencia entre armaduras de materiales compuestos de matriz polimérica (FRP) y hormigón

En este artículo se presentan los resultados del estudio del comportamiento adherente de barras de materiales compuestos de matriz polímero (FRP), con fibras de vidrio (GFRP) y con fibras de carbono (CFRP), como armadura de hormigón. Se realizan un total de 91 ensayos según las normas ACI 440.3R-04 y CSA S806-02. Los parámetros considerados en los ensayos son la resistencia del hormigón,e l acabado superficial,e l tipo de fibra y el diámetro de la barra. Los resultados dan una estimación de la capacidad de adherencia para diferentes tipos de hormigón y armaduras. La diferencia en las propiedades y en el comportamiento adherente se traduce en una respuesta adherencia-deslizamiento distinta