PSI - Issue 36

Petro Yasniy et al. / Procedia Structural Integrity 36 (2022) 197–202 Petro Yasniy, Ihor Okipnyi, Oleksandr Dyvdyk et al. / Structural Integrity Procedia 00 (2021) 000 – 000

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cracked specimen with the expanded hole at the crack tip. Journal of Materials Processing Technology 197(1 – 3), 250 – 254. Buxbaum, O., Huth, H., 1987. Expansion of cracked fastener holes as a measure for extension of lifetime to repair. Engineering Fracture Mechanics 28(5 – 6), 689 – 698. Bahloul, A., Mhalla, M. M., Bouraoui, Ch., 2018. Crack repair of SENT specimen using the interference fit process. Journal of Alloys and Compounds 748, 363 – 374. Burns, S., 2012. Cracks in Airbus A380 Wings Put Pressure on EADS [Electronic resource]. February. FTI Process Specification 8101D, 1994. Fatigue Technology Inc. Gopalakrishna, H. D., Narasimha Murthy, H. N., Krishna, M., 2010. Cold expansion of holes and resulting fatigue life enhancement and residual stresses in Al 2024 T3 alloy – An experimental study. Engineering Failure Analysis 17(2), 361 – 368. Lacarac, V., Smith, D. J., Pavier, M. J., Priest, M., 2000. Fatigue crack growth from plain and cold expanded holes in aluminium alloys. International Journal of Fatigue 22(3), 189 – 203. Laviolette, J., Wing Spar Crack. Feedback, 2012. 2, 5 – 14. Matos, P. F. P. de, McEvily, A. J., Moreira, P. M. G. P., Castro, P.M.S.T. de, 2007. Analysis of the effect of cold-working of rivet holes on the fatigue life of an aluminum alloy. International Journal of Fatigue 29(3), 575 – 586. Seligman, L., Crack Discovered on F-35C Test Plane Wing Spar. Def. News., 2015. November 16. Tajabadi, M., 2016. Case Studies in Engineering Failure Analysis Metallurgical failure analysis of a cracked aluminum 7075 wing internal angle. Case Stud. Eng. Fail. Anal. Elsevier Ltd 7, 9 – 16. Wanlin, G., 1993. Elastic-plastic analysis of a finite sheet with a cold-worked hole. Engineering Fracture Mechanics 45(6), 857 – 864. Warner, J. J., Clark, P. N., Hoeppner, D. W., 2014. Cold expansion effects on cracked fastener holes under constant amplitude and spectrum loading in the 2024-T351 aluminum alloy. International Journal of Fatigue 68, 209 – 216. Yasnii, P. V., Dyvdyk, O. V., Iasnii, V. P., 2020. Modeling of Cold Plastic Deformation of the Holes Made in Specimens of Shape-Memory Alloy. Materials Science 1 – 7. Yasniy, P., Glado, S., Iasnii V., 2017. Lifetime of aircraft alloy plates with cold expanded holes. International Journal of Fatigue 104, 112 – 119. Yasniy, P., Glado, S., Iasnii, V., 2016. Fatigue crack nucleation and propagation in aluminum alloy plates with cold expanded holes. Procedia Structural Integrity 2, 3280 – 3287. Yonezawa, T., Shimanuki, H., Mori, T., 2020. Influence of cyclic loading on the relaxation behavior of compressive residual stress induced by UIT. Welding in the World 64(1), 171 – 178. Zhang, X., Wang, Z., 2003. Fatigue life improvement in fatigue-aged fastener holes using the cold expansion technique. International Journal of Fatigue 25(9 – 11), 1249 – 1257.

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