Issue 52

W. N. Bouzitouna et alii, Frattura ed Integrità Strutturale, 52 (2020) 256-268; DOI: 10.3221/IGF-ESIS.52.20 268 [22] Oudad, W., Belhadri, D. E., Fekirini, H. and Khodja, M. (2017). Analysis of the plastic zone under mixed mode fracture in bonded composite repair of aircraft structures, Aerospace Science and Technology, 69, pp. 404–411. DOI: 10.1016/j.ast.2017.07.001. [23] Thomas, S. B., Mhaiskar, M. J. and Sethuraman, R. (2000). Stress intensity factors for circular hole and inclusion using finite element alternating method, Theoretical and Applied Fracture Mechanics, 33(2), pp. 73–81. DOI: 10.1016/S0167-8442(00)00002-1. [24] Shin, C. (1996). Fatigue damage repair: a comparison of some possible methods, International Journal of Fatigue, 18(8), pp. 535–546. DOI: 10.1016/S0142-1123(96)00029-1. [25] Khoshravan, M. R. and Hamidi, A. (2007). Numerical Analysis of the Influence of Location of the Stopping Holes in the Crack Growth, Journal of Aerospace Science and Technologie, 4(1), pp. 9–16. [26] Gómez, S., Oñoro, J. and Pecharromán, J. (2007). A simple mechanical model of a structural hybrid adhesive/riveted single lap joint, International Journal of Adhesion and Adhesives, 27(4), pp. 263–267. DOI: 10.1016/j.ijadhadh.2006.01.004. [27] Kweon, J.-H., Jung, J.-W., Kim, T.-H., Choi, J.-H. and Kim, D.-H. (2006). Failure of carbon composite-to- aluminum joints with combined mechanical fastening and adhesive bonding, Composite Structures, 75(1–4), pp. 192–198. DOI: 10.1016/j.compstruct.2006.04.013. [28] Chan, W. S. and Vedhagiri, S. (2001). Analysis of Composite Bonded/Bolted Joints Used in Repairing, Journal of Composite Materials, 35(12), pp. 1045–1061. doi: 10.1177/002199801772662325. [29] Hart-Smith, L. J. (1985). Bonded-bolted composite joints, Journal of Aircraft, 22(11), pp. 993–1000. DOI: 10.2514/3.45237. [30] Kanninen, M. F., Broek, D., Marschall, C. W., Rybicki, E. F., Sampath, S. G., Simonen, F. A. and Wilkowski, G. M. (1976). Mechanical fracture predictions for sensitized stainless steel piping with circumferential cracks. [BWR]. [31] Rodriguez, J. E., Brennan, F. P. and Dover, W. D. (1998). Minimization of stress concentration factors in fatigue crack repairs, International Journal of Fatigue, 20(10), pp. 719–725. DOI: 10.1016/S0142-1123(98)00039-5. [32] Ramji, M., Srilakshmi, R. (2012). Design of composite patch reinforcement applied to mixed-mode cracked panel using finite element analysis, J. Reinf. Plast. Compos., 71(2), pp. 258–70, DOI: 10.1177/0731684412440601. [33] Oudad, W., Belhadri, D.E., Fekirini, H. and Khodja, M. (2017). Analysis of the plastic zone under mixed mode fracture in bonded composite repair of aircraft structures, 69, pp. 404–411, DOI: 10.1016/j.ast.2017.07.001.