PSI - Issue 28

A.M. Al-Mukhtar / Procedia Structural Integrity 28 (2020) 124–131 Author name / Structural Integrity Procedia 00 (2019) 000–000

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[15] A. Al-Mukhtar, “Consideration of the residual stress distributions in fatigue crack growth calculations for assessing welded steel joints,” Fatigue Fract. Eng. Mater. Struct. , p. 12060, 2013. [16] A. M. Al-Mukhtar and Q. Doos, “The spot weldability of carbon steel sheet,” Adv. Mater. Sci. Eng. , vol. 2013, 2013. [17] A. M. Al-Mukhtar, “Investigation of the Thickness Effect on the Fatigue Strength Calculation,” J. Fail. Anal. Prev. , vol. 13, no. 1, pp. 63–71, 2013. [18] A. Al Mukhtar, H. Biermann, P. Hübner, and S. Henkel, “Fatigue crack propagation life calculation in welded joints,” in CP2009 , 2013. [19] M. P. Szolwinski and T. N. Farris, “Observation, analysis and prediction of fretting fatigue in 2024 T351 aluminum alloy,” Wear , vol. 221, no. 1, pp. 24–36, Oct. 1998. [20] M. P. Szolwinski and T. N. Farris, “Mechanics of fretting fatigue crack formation,” Wear , vol. 198, no. 1, pp. 93–107, 1996. [21] P. Fromme and M. B. Sayir, “Detection of cracks at rivet holes using guided waves,” Ultrasonics , vol. 40, no. 1–8, pp. 199–203, May 2002. [22] R. Jones, L. Molent, and S. Pitt, “Understanding crack growth in fuselage lap joints,” Theor. Appl. Fract. Mech. , vol. 49, no. 1, pp. 38–50, Feb. 2008. [23] J. H. Park and S. N. Atluri, “Fatigue growth of multiple-cracks near a row of fastener-holes in a fuselage lap-joint,” Comput. Mech. , vol. 13, no. 3, pp. 189–203, 1993. [24] S. J. Findlay and N. D. Harrison, “Why aircraft fail,” Mater. Today , vol. 5, no. 11, pp. 18–25, Nov. 2002. [25] H.-J. Schmidt, “Aircraft fuselage shell component with crack propagation resistance.” Google Patents, 22-Jul-2003. [26] D. Taylor and J. F. Knott, “Fatigue crack propagation behaviour of short cracks; the effect of microstructure,” Fatigue Fract. Eng. Mater. Struct. , vol. 4, no. 2, pp. 147–155, 1981. [27] J. Lankford, “The influence of microstructure on the growth of small fatigue cracks,” Fatigue Fract. Eng. Mater. Struct. , vol. 8, no. 2, pp. 161–175, 1985. [28] A. M. Al-Mukhtar, “Case Studies of Aircraft Fuselage Cracking,” in Advanced Engineering Forum , 2019, vol. 33, pp. 11–18. [29] T. Dursun and C. Soutis, “Recent developments in advanced aircraft aluminium alloys,” Mater. Des. , vol. 56, pp. 862–871, 2014. [30] R. Alessi, “Variational approach to fracture mechanics with plasticity.” Citeseer, 2013. [31] J. C. Newman Jr, X. R. Wu, S. L. Venneri, and C. G. Li, “Small-crack effects in high-strength aluminum alloys,” 1994. [32] J. C. Newman Jr and P. R. Edwards, “Short-crack growth behaviour in an aluminum alloy-an AGARD Cooperative Test Programme,” DTIC Document, 1988.

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