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Fatigue Damage of Rivet Joints in the Condition of Stable Cyclic Load Cover

Fatigue Damage of Rivet Joints in the Condition of Stable Cyclic Load

Open Access
|Sep 2010

References

  1. Li, X. D., & Edwards, L. (1995). Analysis of short crack growth from microscopic fatigue properties. Teoretical and Applied Fracture Mechanics, 23(3), 187-198.10.1016/0167-8442(95)93238-I
  2. Pedro M. G. P. Moreira, Paulo F. P. de Mates & Paulo M. S. T. de Castro. (2005). Fatigue striation spacing and equivalent initial flaw size in Al 2024-T3 riveted specimens. Teoretical and Applied Fracture Mechanics, 43(1), 89-99.10.1016/j.tafmec.2004.12.005
  3. 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.
  4. Kocanda, D., Kocanda, S., & Kulec, P. (2005). Short fatigue crack in 2024-T3 aerospace aluminum alloy sheet. Scientific Papers. Mechanical. Technical University of Opole, 83(2), 83-90.
DOI: https://doi.org/10.2478/v10164-010-0007-9 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 63 - 73
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 Volodymyr Hutsaylyuk, Lucjan Śnieżek, Volodymyr Hlado, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.

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