PSI - Issue 28

Slobodanka Boljanović et al. / Procedia Structural Integrity 28 (2020) 2370 – 2377 Slobodanka Boljanović et al. / Procedia Structural Integrity 00 (2020) 000 – 000

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Acknowledgements The present research was supported by the Serbian Ministry of Education, Science and Technological Development through the Mathematical Institute of the Serbian Academy of Sciences and Arts, Belgrade and the COST Organization, Brussels, Belgium within the Action CA18203, which is gratefully acknowledge. References Antoni, N., Gaisne, F., 2011. Analytical Modelling for State Stress Analysis of Pin-Loaded Lugs with Bush Fitting, Applied Mathematical Modelling 35(1), 1-21. Boljanović, S., Maksimović, S., Carp interi, A., Jovanović, B., 2017 . Computational Fatigue Analysis of the Pin-Loaded Lug with Quarter Elliptical Corner Crack. International Journal of Applied Mechanics 9(4), 1750058:1-17. Carpinteri, A., Handbook of Fatigue Crack: Propagation in Metallic Structures, Amsterdam, Elsevier Science B.V., 1994. Grover, H.J., Hyler, W.S., Kuhn, P., Landers, C.B., Howell, F.M., Axial-Load Fatigue Properties of 24S-T and 75S-T Aluminum Alloy as Determined in Several Laboratories, NASA TN-2928, 1953. Huang, X., Moan, T., 2007. Improved Modeling of the Effect of R -Ratio on Crack Growth Rate. International Journal of Fatigue 29(4), 591 – 602. Kim, J.H., Lee, S.B., Hong, S.G., 2003. Fatigue Crack Growth Behavior of Al7050-T7451 Attachment Lugs under Flight Spectrum Variation. Theoretical and Applied Fracture Mechanics 40(2), 135-144. Newman, Jr. J.C., Raju, I.S., Stress-Intensity Factor Equations for Cracks in Three-Dimensional Finite Bodies Subjected to Tension and Bending Loads, NASA TM-85793, Langley Research Center, Hampton, Virginia, 1984. Song, P., Sheu, B., Shieh, Y., 2002. Prediction of Semi-Elliptical Surface Crack Growth in 2024-T4 Aluninum Alloy. International Journal of Pressure Vessels and Piping 79(4), 273-278. Yamashita, Y., Shinozaki, M., Ueda, Y., Sakano, K., 2004. Fatigue Crack Growth Life Prediction for Surface Crack Located in Stress Concentration Part Based on the Three-Dimensional Finite Element Method. ASME Journal of Engineering for Gas Turbines and Power 126(1), 160-166. Zhan, W., Lu, N., Zhang, C., 2014. A New Approximate Model for the R – Ratio Effect on Fatigue Crack Growth Rate. Engineering Fracture Mechanics 119, 85 – 96.