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Etude expérimentale et modélisation de la durée de vie en fatigue d'un alliage d'aluminium de fonderie A356-T6 sous chargement multiaxial

Abstract : This study aims to investigate the fatigue behaviour of A356-T6 aluminum alloy. Experimental fatigue tests at 106 cycles have been performed for two loading ratios: Rσ = 0 and Rσ = -1. The first experimental investigation was conducted on specimens from a ‘V’ wedge casting with natural and artificial defects which provides a variation of the microstructure. Following the experimental results, we have shown that defects characterized by their size and the microstructure characterized by SDAS, are the main parameters that control the fatigue limit. By comparing the results obtained for both loading ratios, it appears that the mean stress has an effect on the sensitivity to the defect size effect and microstructure.The DSG criterion was modified to introduce the effect of SDAS. This improved DSG criterion has been employed to predict the Kitagawa diagram for multiaxial loading for different loading cases. The simulation of the modified DSG criterion showed that the reduction of the fatigue limit with the defect size and SDAS is well described. In the last part a numerical model was developed to perform a simulation of the fatigue limit starting from the casting process. Using this numerical model, we simulated the defect size and SDAS depending on the solidification time, eventually the fatigue limit issimulated using the improved DSG criterion. With combining between Weibull law and modified DSG,we predict the probability of failure at each point of the structure. We proposed in this part a mold which let to obtain samples with two different microstructures. In this study, a second fatigue tests was carried out on these samples to validate the numerical simulation on the proposed mold. It turns out that the numerical model provides reasonably well the obtained experimental results.
Keywords : Defect size A356-T6
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Submitted on : Thursday, November 19, 2015 - 10:52:08 AM
Last modification on : Wednesday, October 20, 2021 - 3:22:14 AM
Long-term archiving on: : Friday, April 28, 2017 - 2:43:53 PM


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  • HAL Id : tel-01230868, version 1



Mohamed Iben Houria. Etude expérimentale et modélisation de la durée de vie en fatigue d'un alliage d'aluminium de fonderie A356-T6 sous chargement multiaxial. Autre. ISAE-ENSMA Ecole Nationale Supérieure de Mécanique et d'Aérotechique - Poitiers, 2015. Français. ⟨NNT : 2015ESMA0007⟩. ⟨tel-01230868⟩



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