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A prior study conducted by the authors had investigated the behaviour of thin composite double lap joint repairs. This investigation was an extension to the previous study and focused on analysing the behaviour of thick step lap joint repairs which are more complicated in nature. Finite element analysis (FEA) was performed to verify the static and fatigue strength of bolted, bonded and hybrid joint...
Fibre reinforced polymer matrix composites are being increasingly used for aircraft structures because of their superior structural performance, such as high strength, high stiffness, long fatigue life, and low density. This study is targeted towards the repair of thicker composite step lap joint configurations. The aim is to compare the static strength and fatigue resistance of a hybrid joint consisting...
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