A link-up resulted fatigue crack branching in Al–Cu–Mg alloy-Reference-Cited by-同舟云学术

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A link-up resulted fatigue crack branching in Al–Cu–Mg alloy

Published:2016-11 Issue: Volume:92 Page:459-469
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Lu Songsong^ORCID,Bao Rui,Zhang Ting,Fei Binjun

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modelling and Simulation

Reference27 articles.

1. Aluminium alloys – a century of age hardening;Polmear;Mater Forum,2004

2. Development of high performance aluminium alloy sacrificial anodes reinforced with metal oxides;Shibli;Mater Lett,2007

3. Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material;Johnston,2001

4. Fracture testing of 2324-T39 aluminum alloy;Dawicke,1995

5. Fatigue crack growth in 2324 aluminium alloy;Mallory;J Young Investigator,2006

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1. Study of fatigue crack growth behaviour of Al-Mg and Al-Mg-Sc-Zr alloys;Materials Science and Technology;2023-06

2. Fe-rich particles influenced secondary crack characteristics in an Al-Zn-Mg-Cu alloy extrusion plate with high zinc content;Scripta Materialia;2020-09

3. Modeling approach for a unified crack growth model in short and long fatigue crack regimes;International Journal of Fatigue;2019-11

4. Low anisotropy of fatigue crack growth in Al-5.8Mg-0.25Sc;International Journal of Fatigue;2019-08

5. Trends in fatigue-crack growth for the 2024 Al-alloy after a single tensile overload;Materiali in tehnologije;2018-12-17

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