Issue 46

N. C. M. Ibrahim et alii, Frattura ed Integrità Strutturale, 46 (2018) 140-149; DOI: 10.3221/IGF-ESIS.46.14 149 [9] Young. A, Rooke, D. P. and Cartwright, D.J. (1989). Numerical Study of Balanced Patch Repairs to Cracked Sheet. Aero. J., pp. 327- 334. DOI: 10.1017/S0001924000017255. [10] Rooke, D. P., Young, A. and Courtney, T.J. (1992). Effect of Repair Patches on Fatigue Lifetimes. Durability of Metal Aircraft Structures, Ed: Atluri, S. N., Harris, C.E., Hoggard, A., Miller, N/ and Sampath, S. G., Atlanta Technology Publications, pp. 132-145. [11] Ramesh C., Murthy, M. V. V., Ramamurthy, T. S. and Rao, A. K. (1985). Analytical Estimation of Stress Intensity Factors in Patched Cracked Plates. Eng. Frac. Mech., 21, pp. 479-494. DOI: 10.1016/S0013-7944(85)80041-2. [12] Liu, T. and Fan, W. (1994). Analysis for an Adhesively Bonded Finite Strip Repair to a Cracked Plate. Eng. Frac. Mech., 47, pp. 629-637. DOI: 10.1016/0013-7944(94)90154-6. [13] Arendt, C. and Sun, C. T. (1994). Bending Effects of Unsymmetric Adhesively Bonded Composite Repairs on Cracked Aluminium Panels. NASA CP 3274, pp. 33-48. [14] Fekirini, H., Bouiadjra, B. B., Belhouari, M., Boutabout, B., Serier, B. (2008). Numerical analysis of the performances of bonded composite repair with two adhesive bands in aircraft structures, Composite structures, pp. 8284-8289. DOI: 10.1016/j.compstruct.2006.12.004. [15] Belhouari, B. B. and Serier, B., (2004). Comparison of double and single bonded repairs to symmetric composite structures: A numerical analysis, composite Structures, 65, pp. 47–53. DOI: 10.1016/j.compstruct.2003.10.005. [16] Bachir B. B., Belhouari, M. and Serier, B. (2002). Computation of the stress intensity factors for repaired cracks with bonded composite patch in mode I and mixed mode. Composite Structures, 56, pp. 401 - 406. DOI: 10.1016/S0263-8223(02)00023-5. [17] Ouinas, D., Bouiadjra, B.B., Serier, B. and Said Bekkouche, M. (2007). The effects of disbands on the stress intensity factor of aluminium panels repaired using composite materials. Compos Struct. 78, pp. 278–84. DOI: 10.1016/j.commatsci.2006.09.006. [18] Ouinas, D., Hebbar, A. and Vina Olay J. (2006). Fracture Mechanics Modelling of Cracked Aluminium Panel Repaired with Bonded Composite Circular Patch. Journal of Applied Science 9, pp. 2088-2095. DOI: 10.3923/jas.2006.2088.2095 [19] Ouinas D., Ramdane, Z. and Sahnoun M. (2011). Effet de la forme géométrique du patch sur la réduction du FIC en mode I. Journées d’Etudes Nationales de Mécanique, JENM’2011 Ouargla, Algérie. [20] Mhamdia, R., Bouiadjra, B.B., Serier, B. and Belhouari, M. (2012). The Patch Shape Effects on the Performances of Bonded Composite Repair in Aircraft Structures. Proceedings of the International Conference on Industrial Engineering and Operations Management Istanbul, Turkey.

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