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A Model for Fatigue Crack Growth in the Paris Regime under the Variability of Cyclic Hardening and Elastic Properties Cover

A Model for Fatigue Crack Growth in the Paris Regime under the Variability of Cyclic Hardening and Elastic Properties

Fatigue of Aircraft Structures
Volume 2017 (2017): Issue 9 (December 2017)
By: Tayeb Kebir,  Mohamed Benguediab and  Abdellatif Imad  
Open Access
|Aug 2018

Authors

Tayeb Kebir

Department of Mechanical Engineering, Faculty of Technology, Laboratory of Materials and Reactive Systems (LMRS), University of Sidi Bel-Abbes, Algeria

Mohamed Benguediab

Department of Mechanical Engineering, Faculty of Technology, Laboratory of Materials and Reactive Systems (LMRS), University of Sidi Bel-Abbes, Algeria

Abdellatif Imad

Polytech’Lille1, Laboratory of Mechanical of Lille (LML), University of Lille1, France
DOI: https://doi.org/10.1515/fas-2017-0010 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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Language: English
Page range: 117 - 135
Published on: Aug 9, 2018
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
Keywords:
cyclic plastic strain,
elastic properties,
cyclic hardening parameters,
Young’s modulus,
variability,
crack tip,
fatigue crack growth,
constants of the Paris law,
Al-alloys
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2018 Tayeb Kebir, Mohamed Benguediab, Abdellatif Imad, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

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