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A Finite Element Model for Predicting the Static Strength of a Composite Hybrid Joint with Reinforcement Pins
Francesco Bianchi1, Yiding Liu2, Adam M Joesbury1
1Composites and Advanced Materials Centre, School of Aerospace, Transport and Manufacturing, Cranfield University, Bedford MK43 0AL, UK.
Abstract:
This paper presents a finite element model for predicting the performance and failure behaviour of a hybrid joint assembling fibrous composites to a metal part with reinforcement micro pins for enhancing the damage tolerance performance. A unit-strip model using the cohesive elements at the bond interface is employed to simulate the onset and propagation of debonding cracks. Two different traction-separation laws for the interface cohesive elements are employed, representing the fracture toughness properties of the plain adhesive bond and a pin-reinforced interface, respectively. This approach can account for the large-scale crack-bridging effect of the pins. It avoids using concentrated pin forces in the numerical model, thus removing mesh-size dependency, and permitting more accurate and robust computational analysis. Lap joints reinforced with various pin arrays were tested under quasi-static load. Predicted load versus applied displacement relations are in good agreement with the test results, especially for the debonding onset and early stage of crack propagation.
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