Browsing by Author "De Francisco, Unai"
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Item Cohesive zone modelling of hydrogen environmentally assisted cracking for double cantilever beam samples of 7xxx aluminium alloys(2024-10) De Francisco, Unai; Larrosa, Nicolas O.; Peel, Matthew J.; MATERIALES PARA CONDICIONES EXTREMASDouble cantilever beam (DCB) samples are typically used to estimate the crack growth rates during hydrogen environmentally assisted cracking (HEAC) of 7xxx aluminium alloys. In this investigation, a cohesive zone model was developed to simulate the HEAC behaviour of 7xxx alloys during DCB tests. A coupled mass-diffusion and stress analysis was performed in Abaqus to elucidate key parameters affecting crack growth rates via sensitivity analysis. The threshold stress intensity for cracking was mainly dependent on hydrogen solubility, while the stage II crack growth rate was influenced by the mass-transfer coefficient and diffusivity. Model parameters were fitted to match experimental results of AA7449-T7651 at different temperatures, analysing hydrogen distribution within the samples. Results indicated that hydrogen concentration at external and fractured surfaces remained at saturation levels throughout the tests. The postulated crack propagation mechanism involves enhanced hydrogen diffusion near the crack tip due to a high hydrogen concentration gradient, crack growth driven by hydrogen accumulation, and enhanced hydrogen ingress at newly formed surfaces.Item The influence of temperature on hydrogen environmentally assisted cracking of AA7449-T7651 in moist air(2021-03) De Francisco, Unai; Larrosa, Nicolas O.; Peel, Matthew J.; MATERIALES PARA CONDICIONES EXTREMASThe 7xxx series of aluminium alloys are sensitive to intergranular hydrogen environmentally assisted cracking (HEAC) in moist air environments. A new generation of 7xxx alloys used in aircraft components (including AA7449) have been found to be more sensitive to HEAC. This investigation aims to quantify the HEAC crack growth rates of AA7449-T7651 in moist air at different temperatures. Double cantilever beam specimens were loaded at a constant displacement and placed in moist air (80–85% relative humidity) at temperatures between 25 and 80 °C. Regular measurements of crack length permitted the determination of the crack growth rate as a function of the stress intensity factor (KI) during stage I (high KI dependence of growth rate) and stage II (low KI dependence of growth rate). Increasing the temperature was found to increase the crack growth rate during stage II cracking, following Arrhenius kinetics. The activation energy for the stage II crack growth rate at a stress intensity factor of 14.5 MPam was estimated as 84.7 kJ/mol. Additionally, the threshold stress intensity factor for HEAC was found to decrease with increasing temperature. This was attributed to a higher hydrogen solubility at higher temperatures. The crack growth rate of AA7449-T7651 at room temperature was similar to that of overaged AA7050 and AA7075-T7651, ranging between 1.3 and 2.1 × 10−7 mm/s. It was inferred that the alloy temper has more influence than the composition during stage II cracking at room temperature.