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New methodology of dynamical material response of dissimilar FSWed Al alloy joint under high strain rate laser shock loading

Article dans une revue avec comité de lecture
Author
AYAD, Mohammad
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
LAPOSTOLLE, Lucas
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
RONDEPIERRE, Alexandre
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
530280 Thales LAS France
BRAS, Corentin Le
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
254102 Airbus Operation S.A.S.
ÜNALDI, Selen
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
DONIK, Črtomir
KLOBČAR, Damjan
BERTHE, Laurent
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
TRDAN, Uroš
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]

URI
http://hdl.handle.net/10985/22781
DOI
10.1016/j.matdes.2022.111080
Date
2022-08
Journal
Materials and design

Abstract

This paper presents an innovative methodology of material characterization under high strain rate (order of 107s��1) laser shock loading coupled with microstructural and mechanical material features. To that scope, experimental and simulation analyses have been conducted for Al alloys (AA7075-T6 and AA2017-T4) and dissimilar Friction Stir Welded (FSWed) AA7075-AA2017 joint, under shock pressure of 4.5 GPa (laser power density of 3.5 GW=cm2). In order to perform proper in-depth material model sim-ulation of these alloys and dissimilar pairs, Johnson–Cook (J-C) material model has been coupled with Grüneisen equation of state using the non-linear explicit code LS-DYNA. For the first time, we provided a way to differentiate between material behaviour in the cross-section and the in-plane rolling and weld-ing direction. What is more, we have provided the link between microstructural features and mechanical properties such as microhardness, residual stresses and the identified material parameters. By achieving this goal, the bigger difference between studied planes was confirmed for strain hardening modulus, strain hardening exponent and strain rate sensitivity parameters. Obtained results and proposed method-ology indicate high potential to predict material properties and behaviour of dynamically stressed parts and at the same time can be used for optimization of LSP process.

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