Issue 78

S. Vantadori et alii, Fracture and Structural Integrity, 78 (2026) 432-453; DOI: 10.3221/IGF-ESIS.78.25

[36] Bianchetti, C., Zheng, R., Chromik, R.R., Lévesque, M., Brochu, M. (2018). Comparison of small and long fatigue crack growth behavior in AA 7050-T7451. Engineering Fracture Mechanics, 202, pp. 20-32. [37] Newman, J.C., Jr., Walker, K.F. (2019). Fatigue-crack growth in two aluminum alloys and crack-closure analyses under constant-amplitude and spectrum loading. Theoretical and Applied Fracture Mechanics, 100, pp. 307-318. [38] Borrego, L.P., Jesus, J.S., Branco, R., Ferreira, J.A.M., Antunes, F.V., Neto, D.M., Sérgio, E.R. (2025). Mechanisms of fatigue crack growth in 7050-T6 aluminium alloy. International Journal of Fatigue, 194, 108830. [39] Sharma, V., Mallick, A., Gupta, M. (2023). Enhancing significantly the strength and tribological response of Al7075 alloy using nano-ZrO2 reinforcement. Journal of Materials Research and Technology, 27, pp. 7280-7292. [40] Oskouei, R.H., Ibrahim, R.N. (2011). The effect of a heat treatment on improving the fatigue properties of aluminium alloy 7075-T6 coated with TiN by PVD. Procedia Engineering, 10, pp. 1936-1942. [41] DeBartolo, E.A., Hillberry, B.M. (2001). A model of initial flaw sizes in aluminum alloys. International Journal of Fatigue, 23 (SUPPL. 1), pp. 79-86.

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