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Fractographic analysis of the overload effect on fatigue crack growth in 2024-T3 and 7075-T6 Al alloys

  • A. AlbedahEmail author
  • B. Bachir Bouiadjra
  • S. M. A. K. Mohammed
  • F. Benyahia
Article
  • 11 Downloads

Abstract

The effect of single overload on the fatigue crack growth in 2024-T3 and 7075-T6 Al alloys was analyzed. Fatigue tests under constant-amplitude loading with overload peak were carried out on V-notched specimens. Fractographic analysis was used as a principal approach to explain the crack growth retardation due to the overload. Scanning electron microscopy (SEM) analyses were conducted on the fractured surface of failed specimens to study the retardation effect. The obtained results show that the overload application generates a plastic zone in both aluminum alloys. The generated plastic zone is three times larger in the case of 2024-T3 compared to 7075-T6, and thus, a significant crack retardation was induced for 2024-T3. The retardation effect due to the overload for 2024-T3 and 7075-T6 lasted for about 10 mm and 1 mm, respectively, from the point of overload application.

Keywords

fatigue crack growth overload retardation fractography crack tip plasticity 

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Notes

Acknowledgement

The authors extend their appreciation to the Deanship of Scientific Research at King Saud University for funding the work through the research group (No. RGP-VPP-035).

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Copyright information

© University of Science and Technology Beijing and Springer-Verlag GmbH Germany, part of Springer Nature 2020

Authors and Affiliations

  • A. Albedah
    • 1
    Email author
  • B. Bachir Bouiadjra
    • 1
    • 2
  • S. M. A. K. Mohammed
    • 1
    • 3
  • F. Benyahia
    • 1
  1. 1.Mechanical Engineering Department, College of EngineeringKing Saud UniversityRiyadhSaudi Arabia
  2. 2.LMPM, Department of Mechanical EngineeringUniversity of Sidi Bel AbbesSidi Bel AbbesAlgeria
  3. 3.Department of Mechanical and Industrial EngineeringRyerson UniversityTorontoCanada

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