Issue 43

F.Z. Seriari et alii, Frattura ed Integrità Strutturale, 43 (2018) 43-56; DOI: 10.3221/IGF-ESIS.43.03 54 [4] Baker, A.A., Crack patching: experimental studies, practical applications. In: A.A. Baker and R. Jones (eds), Bonded repair of aircraft structures. Dordrecht (NL): Martinus Nijhoff Publishers (1988) 107-173. [5] Woerden, H.M., Mortier, W.J., Guijt, C.B., Verhoeven, S., Bonded repair patches. In: A. Vlot et al. (eds.), Fibre Metal Laminates, Kluwer Academic Publishers (2001). [6] Sabelkin, V., Mall, S., Hansen, M.A., Vandawaker, R.M., Derriso, M., Investigation into cracked aluminum plate repaired with bonded composite patch. Composite Structures 79 (2007) 55–66. DOI: 10.1016/j.compstruct.2005.11.028. [7] Tsamasphyros, G.J., Kanderakis, G.N., Karalekas, D., Rapti, D., Gdoutos, E.E., Zacharopoulos, D., Marioli-Riga, Z.P., Study of composite patch repair by analytical and numerical methods. Fatigue Fract Engng Mater Struct 24 (2001) 631–636. DOI: 10.1046/j.1460-2695.2001.00414.x/abstract. [8] Costa, M., Viana, G., da Silva, L.F.M., Campillo, R.D.S.G., Effect of humidity on the fatigue behaviour of adhesively bonded aluminium joints. Latin American Journal of Solids and Structures 14 (2017) 174-187. [9] Negru, R., Serban, D.A., Marsavina, L., Magda, A., Lifetime prediction in medium-cycle fatigue regime of notched specimens. Theoretical and Applied Fracture Mechanics, 84 (August 2016), 140-148. DOI: 10.1016/j.tafmec.2016.03.006. [10] Sabelkin, V., Mall, S. Avram, J.B., Fatigue crack growth analysis of stiffened cracked panel repaired with bonded composite patch. Engineering Fracture Mechanics 73 (2006) 1553-67. DOI: 10.1016/j.engfracmech.2006.01.029 [11] Marsavina, L., Sadowski, T., Knec, M. Crack propagation paths in four point bend Aluminium–PMMA specimens. Engineering Fracture Mechanics, 108 (August 2013), 139-151. DOI: 10.1016/j.engfracmech.2013.02.029. [12] Salehi-Khojin, A., Thoreson, A.R., Zhong, W.H., Stone, J.J., Gan, Y.X., The effect of patch geometry on the static and fatigue behaviors of defective aluminum panels repaired with a composite patch, Journal of Adhesion Science and Technology 20(6) (2006) 537-554. DOI: 10.1163/156856106777213311. [13] Ricci, F., Franco, F., Montefusco, N., Experimental and numerical analysis of the fatigue behaviour of panels repaired by patches in composite material. Key Engineering Materials, 417-418 (2010) 597-600. DOI: 10.4028 /www.scientific.net/KEM.417-418.597. [14] Schubbe, J.J., Bolstad, S.H., Reyes, S., Fatigue crack growth behavior of aerospace and ship-grade aluminum repaired with composite patches in a corrosive environment, Composite Structures 144 (2016) 44–56. DOI: 10.1016/j.compstruct.2016.01.107. [15] Klug, C., Sun, C.T., Large deflection effects of cracked aluminum plates repaired with bonded composites patches, Composite Structures 42 (1988) 291–296. DOI: 10.1016/S0263-8223(98)00018-X. [16] Duquesnay, D.L., Underhill, P.R., Britt, H.J., Fatigue failure of adhesively patched 2024-T3 and 7075-T6 clad and bare aluminium alloys, Fatigue Fract Engng Mater Struct 28 (2005) 381-389. DOI: 10.1111/j.1460-2695.2005.00869.x/abstract. [17] Hosseini-Toudeshky, H., Effects of composite patches on fatigue crack propagation of single-side repaired aluminum panels. Composite Structures 76 (2006) 243–251. DOI: 10.1016/j.compstruct.2006.06.028. [18] Pastor, M.L., Balandraud, X., Robert, J.L. Grediac, M., Lifetime prediction of aluminium structures reinforced with composite patches. International Journal of Fatigue 31(2009) 850-58. DOI: 10.1016/j.ijfatigue.2008.11.009. [19] Mall, S., Schubbe, J.J., Bonded composite patch geometry effects on fatigue crack growth in thin and thick aluminum panels. Tech Science Press, SL: Structural Longevity 2(1) (2009) 25-47. [20] Dawicke, D.S., Overload and underload effects on the fatigue crack growth behaviour of the 2024-T3 aluminum alloy. NASA Contractor Report 201668, Dawicke Analytical Services & Materials, Inc., Hampton, Virginia (1997). [21] Corbley, D.M., Packman, P.F., On the influence of single and multiple peak overloads on fatigue crack propagation in 7075 T6511 aluminum, Engineering Fracture Mechanics 5(1973) 479-497. DOI: 10.1016/0013-7944(73)90034-9. [22] Kermanidis, A.T., Pantelakisn, S.G., Prediction of crack growth following a single overload in Al-alloy with sheet and plate microstructure. Engineering Fracture Mechanics 78 (2011) 2325-2337. DOI: 10.1016/j.engfracmech.2011.05.005. [23] Wang, C., Wang, X., Ding, Z., Xu, Y., Gao, Z., Experimental investigation and numerical prediction of fatigue crack growth of 2024-T4 aluminum alloy, International Journal of Fatigue 78(2015) 11-21. DOI: 10.1016/j.ijfatigue.2015.03.024. [24] Albedah, A., Khan, S.M.A., Benyahia, F., Bachir Bouiadjra, B., Experimental analysis of the fatigue life of repaired cracked plate in aluminum alloy 7075 with bonded composite patch, Engineering Fracture Mechanics 145 (2015) 210- 220. DOI: 10.1016/j.engfracmech.2015.04.008. [25] Albedah, A., Khan, S.M.A., Benyahia, F., Bachir Bouiadjra, B., Effect of load amplitude change on the fatigue life of cracked Al plate repaired with composite patch, International Journal of Fatigue 88 (2016) 1-9. DOI: 10.1016/j.ijfatigue.2016.03.002.