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Weibull or Lognormal Distribution to Characterize Fatigue Life Scatter – Which is More Suitable? – Continued Cover

Weibull or Lognormal Distribution to Characterize Fatigue Life Scatter – Which is More Suitable? – Continued

Open Access
|Jul 2025

References

  1. Abernethy, R. B. (2006). The new weibull handbook, 5th edition. Abernethy.
  2. Brot, A. (2017). Plantema memorial lecture - three faces of aeronautical fatigue. In Proceedings of the 29th ICAF symposium, Nagoya, Japan (pp. 1186–1225). VTT Information Service.
  3. Brot, A. (2019). Weibull or log-normal distribution to characterize fatigue life scatter –which is more suitable? In A. Niepokolczycki & J. Komorowski (Eds.), ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing. ICAF 2019. Lecture Notes in Mechanical Engineering (pp. 551–561). Springer, Cham. https://doi.org/10.1007/978-3-030-21503-3_44
  4. Brot, A. (2019). Weibull or log-normal distribution to characterize fatigue life scatter –which is more suitable? 30th ICAF Symposium presentation slides, following correspondence with Brot.
  5. Goranson, U. G. (1997). Fatigue issues in aircraft maintenance and repairs. International Journal of Fatigue, 19(93), 3–21. https://doi.org/10.1016/s0142-1123(97)90029-3
  6. ReliaSoft. (2024). Life Data Analysis Reference. https://help.reliasoft.com/reference/life_data_analysis/pdfs/lda_ref.pdf
  7. Schijve, J. (1992). A normal distribution or a weibull distribution for fatigue lives (LR-689). Delft University of Technology, Netherlands.
  8. Schijve, J. (2009). Fatigue of structures and materials, 2nd edition. Springer.
  9. Schijve, J., & Jacobs, F. A. (1955). Fatigue tests on notched and unnotched clad 24 S-T sheet specimens to verify the cumulative damage hypothesis (M-1982). Nat. Aerospace Laboratory, Netherlands.
  10. Whittaker, I. C. (1972). Development of titanium and steel fatigue variability model for application of reliability analysis approach to aircraft structures (Technical Report AFML-TR-72-236). The Boeing Company.
  11. Whittaker, I. C., & Besuner, P. M. (1969). A reliability analysis approach to fatigue life variability of aircraft structures (Technical Report AFML-TR-69-65). The Boeing Company.
DOI: https://doi.org/10.2478/fas-2024-0011 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 131 - 146
Published on: Jul 7, 2025
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2025 Rob Plaskitt, Chris Wynn-Jones, Andrew Halfpenny, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.