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Analysing Micromechanisms of Initiation and Propagation of Short Fatigue Cracks from Rivet Holes in the Aluminums Sheets Cover

Analysing Micromechanisms of Initiation and Propagation of Short Fatigue Cracks from Rivet Holes in the Aluminums Sheets

Open Access
|Sep 2010

References

  1. Paris, P., & Erdogan, F. (1963). A critical analysis of crack propagation laws. Journal of Basic Engineering. 85(4), 60-68.10.1115/1.3656900
  2. Miller, K. J. (1993). Materials science perspective of metal fatigue resistance. Materials science and technology. 9, 453-462.10.1179/mst.1993.9.6.453
  3. Newman, J. C., Phillips, E. P., & Swain, M. H. (1999). Fatigue life prediction methodology using small-crack theory, International Journal of Fatigue, 21(2), 109-119.10.1016/S0142-1123(98)00058-9
  4. Laz, P. J., & Hillberry, B. M. (1998). Fatigue life prediction from inclusion initiated cracks. International Journal of Fatigue, 20(4), 263-271.10.1016/S0142-1123(97)00136-9
  5. Kocanda, D., Kocanda, S., & Torzewski, J. (2003). Variable Amplitude Load Interaction in Fatigue Crack Growth for 2024-T3 Aluminium. Transactions of the Kielce University of Technology, 78, 269-278.
  6. Romaniv, O. N., Yarema, S. Ya., Nikiforchin, G. N., Makhutov, N. A., & Stadnik, M. M. (1990). Fatigue and Cyclic Crack-Growth Resistance of Structural Materials. In: Panasyuk V. V. (Eds.), Fracture Mechanics and Strength of Materials. A Handbook [in Russian], 4, Kyiv: Naukova Dumka.
  7. Kocanda, D., Hutsaylyuk, V., & Hlado, V. (2007). Analize propagation short fatigue crack from hole and micromechanism fracture lamer sheet aluminium alloy 2024-T3. Military University of Technology WAT Bulletin, 56(4), 37-54.
  8. Halliday, M. D., Cooper, C., Poole, P., & Bowen, P. (2003). On predicting small fatigue crack growth and fatigue life from long crack data in 2024 aluminium alloy. International Journal of Fatigue, 25(8), 709-718.10.1016/S0142-1123(03)00052-5
  9. Kocanda, D., Kocanda, S., & Kulec, P. (2005). Short fatigue crack in avia aluminum alloy 2024-T3. Scientific Papers. Mechanics [in Polish]. Technical University of Opole, 83(2), 83-90.
  10. Li, X. D. (1996). Micromechanical model of stage I to stage II crack growth transition for aluminium alloys. Theoretical and Applied Fracture Mechanics, 24, 217-231.10.1016/0167-8442(95)00045-3
DOI: https://doi.org/10.2478/v10164-010-0009-7 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 84 - 101
Published on: Sep 23, 2010
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2010 Dorota Kocańda, Volodymyr Hutsaylyuk, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.

Volume 2009 (2009): Issue 1 (July 2009)