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Predicting Fatigue Crack Growth and Fatigue Life Under Variable Amplitude Loading Cover

Predicting Fatigue Crack Growth and Fatigue Life Under Variable Amplitude Loading

Open Access
|Dec 2010

References

  1. D. Kocańda, J. Torzewski, Prediction of fatigue crack growth for 2024-T3 aluminium alloy under block program loading, Biull. MUT Warsaw, Vol. LVI 4, 2007, pp. 37-55 (in Polish).
  2. J. Torzewski, Fatigue crack growth rate and the ability of its reconstruction on the basis of the fractographic analysis for 2024-T3 aluminium alloy sheet subjected to program loadings, Ph.D. Thesis, MUT, Warsaw 2007 (in Polish).
  3. A. Rama Chandra Murthy, G.S. Palani, Nagesh R. Iyer, An improved Wheeler model for remaining life prediction of cracked plate panels under tensile-compressive overloading. SID Vol. 1, No 3, 2005, pp. 203-213.
  4. H. Tomaszek, J. Żurek, M. Jasztal, Forecasting of damage menaced the safety of aircraft flights. ITE-PIB Radom 2008, (in Polish).
DOI: https://doi.org/10.2478/v10164-010-0024-8 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 37 - 51
Published on: Dec 20, 2010
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2010 Michal Jasztal, Dorota Kocanda, Henryk Tomaszek, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.