PSI - Issue 66

Slobodanka Boljanović et al. / Procedia Structural Integrity 66 (2024) 535– 542 S. Boljanovi ć and A. Carpinteri/ Structural Integrity Procedia 00 (2025) 000–000

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Acknowledgements The present research work 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, which is gratefully acknowledge. References Ahn, S.H., Ando, K., Hidaka, A., 1997. Fatigue Crack Growth and Penetration Behaviour in a Pipe Subjected to Bending Load. In: Proceedings of International Conference on Importance of Understanding the Fundamentals of the Fatigue Process in Counteracting its Effects in Engineering Components and Structures, Sheffield, 17-21 March, pp.73-82. Boljanovi ć , S., Maksimovi ć , S., Carpinteri, A., Jovanovi ć , 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. Boljanovi ć , S., Maksimovi ć , S., Carpinteri, A., Ć osi ć , M., 2019. Fatigue Endurance Design of Plates with Two Semicircular Edge Notches and One Quarter-Elliptical Corner Crack or Through-The-Thickness Crack. International Journal of Fatigue 127, 45-52. Boljanovi ć , S., Carpinteri, A., 2021. Modelling of the Fatigue Strength Degradation Due to a Semi-Elliptical Flaw. Forces in Mechanics 4, 100020. Carpinteri, A. Handbook of Fatigue Crack: Propagation in Metallic Structures, Amsterdam, Elsevier Science B.V., 1994. Hall, L.R., Shah, R.C., Engstrom, W.L. Fracture and Fatigue Crack Growth Behavior of Surface Flaws and Flaws originating at Fastener Holes, AFFDL-TR-74-47, Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Flight Base, Ohio, 1974. Jones, R., Peng, D., Pitt, S., Wallbrik, C .2004. Weight Functions, CTOD, and Related Solutions for Cracks at Notches. Engineering Failure Analysis 11(1), 79-114. Kujawski, D., 2001. A New (  K + K max ) 0.5 Driving Force Parameter for Crack Growth in Aluminium Alloys. International Journal of Fatigue 23, 733–740. Huang, X., Moan, T., 2007. Improved Modeling of the Effect of R -Ratio on Crack Growth Rate. International Journal of Fatigue 29, 591–602. Mikheevskiy, S., Glinka, G., Algera, D., 2012. Analysis of Fatigue Crack Growth in an Attachment Lug Based on the Weight Function Technique and the UniGrow Fatigue Crack Growth Model. International Journal of Fatigue 42, 88–94. Newman, J.C., Jr., 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. Noroozi, A.H., Glinka, G., Lambert, S., 2007. A Study of the Stress Ratio Effects on Fatigue Crack Growth Using the Unified Two-Parameter Fatigue Crack Driving Force. International Journal of Fatigue 29, 1616–1633. Peng, D., Wallbrink, C., Jones, R. 2005. An Assessment of Stress Intensity Factors for Surface Flaws in a Tubular Member, Engineering Fracture Mechanics 72, 357-371. Putra, I.S., Schijve, J. 1992. Crack Opening Stress Measurements of Surface Cracks in 7075-T6 Aluminium Alloy Plate Specimen Through Electron Fractography. Fatigue and Fracture of Engineering Materials and Structures 15(4), 323-338. Smith, R.A., Cooper, J.F. 1989. A Finite Element Model for the Shape Development of Irregular Planar Cracks, International Journal of Pressure Vessels and Piping 36(4), 315-326. 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.