Abstract
In this paper, numerical investigation was carried out to quantify the effect of the cold expansion on fatigue crack initiation in Aluminium alloy. The improvement in fatigue initiation life of specimen after the cold expansion process was investigated with the drilled hole of 2024 T351 Aluminium alloy plate. The 4.6 % in degree of expansion is applied witch is associated with the effect of friction (µ=0.2). Residual stress field is determined using 3D Finite Element Analysis and shows the presence of compressive residual stress around the hole. The results showed a high level of compressive residual stress in mild and exit face of hole. Local strain approach is applied in evaluation of fatigue initiation lives under Afgrow environment code. Fatigue initiation lives are improved by the presence of compressive residual and comparatively to the drilled hole. Moreover, increasing in stress ratio, increases the fatigue initiation lives with and without the presence of compressive residuals stresses
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Article history
- ReceivedUntil the next stage: 36 days
- Revision requestedUntil the next stage: 3 days
- AcceptedUntil the next stage: 176 days
- Published
About the authors
Mohamed El Habiri
Phd Student in Materials Sciences
Mustapha Benachour
Professor and Researcher in Materials Sciences and Mechanical Engineering.
Research in fatigue, fracture of materials, Alloys and Welded materials including residual stresses
Nadjia Benachour
Doctor in Physics and Materials Sciences
Department of Physics
Lecturer
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Copyright © 2018 Mohamed EL HABIRI, Mustapha BENACHOUR, Nadjia BENACHOUR.
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