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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Breitbarth, Eric
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (10/10 displayed)
- 2024An iterative crack tip correction algorithm discovered by physical deep symbolic regressioncitations
- 2024Numerical Simulations of Stress Intensity Factors and Fatigue Life in L-Shaped Sheet Profilescitations
- 2024Next generation fatigue crack growth experiments of aerospace materialscitations
- 2023Werkstoffmechanische Prüfung der nächsten Generation: Rissfortschritt komplexer Rumpfstrukturen
- 2023Strategies to accelerate the design, discovery, development and deployment of materials in the era of the digital transformation
- 2023Fatigue crack growth in anisotropic aluminium sheets–phase-field modelling and experimental validationcitations
- 2022Towards three dimensional aspects of plasticity-induced crack closure: A finite element simulationcitations
- 2022Damage Mechanisms and Anisotropy of an AA7010-T7452 Open-Die Forged Alloy: Fatigue Crack Propagationcitations
- 2020High-stress fatigue crack propagation in thin AA2024-T3 sheet materialcitations
- 2019Anisotropes Rissausbreitungsverhalten einer freiformgeschmiedeten, hochfesten AA7010-T7652 Legierung
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article
Fatigue crack growth in anisotropic aluminium sheets–phase-field modelling and experimental validation
Abstract
Fatigue crack growth is decisive for the design of thin-walled structures such as fuselage shells of air planes. The cold rolling process, used to produce the aluminium sheets this structure is made of, leads to anisotropic mechanical properties. In this contribution, we simulate the fatigue crack growth with a phase-field model due to its superior ability to model arbitrary crack paths. A fatigue variable based on the Local Strain Approach describes the progressive weakening of the crack resistance. Anisotropy regarding the fracture toughness is included through a structural tensor in the crack surface density. The model is parameterised for an aluminium AA2024-T351 sheet material. Validation with a set of experiments shows that the fitted model can reproduce key characteristics of a growing fatigue crack, including crack path direction and growth rate, considering the rolling direction.