[1] Duong, C.N. and Wang, C.H., "Composite Repair: Theory and design", Elsevier, Oxford, pp. 1-8, 2007.
[2] Baker, A. and Jones, R., "Bonded repair of aircraft structures", Dordrecht, Martinus Nijhoff, 1988.
[3] Ratwani, M.M. and Kan, H.P., "Analysis of Cracked, Adhesively Bonded Laminated Structures", AIAA Journal, Vol. 17, No. 9, pp. 988-994, 1979.
[4] Rose, L.R.F., "An application of the inclusion analogy for bonded reinforcements", International Journal of Solids and Structures, Vol. 17, pp. 827–838, 1981.
[5] Rose, L.R.F., "A cracked plate repaired by bonded reinforcements" International Journal of Fracture, Vol. 18, pp. 135–144, 1982.
[6] Rose, L.R.F., "Theoretical analysis of crack patching. In Bonded Repair of Aircraft Structure", Kluwer Academic Publisher, pp. 77–106, 1988.
[7] Atluri, S.N., "Composite Repairs of Cracked Metallic Aircraft Structures", Dept. of Transportation Repport No.DOT/FAA/CT-92/32, 1992.
[8] Bottega, W.J. and Loia, M.A., "Edge debonding in patched cylindrical panels" International Journal of Solids and Structures, Vol. 33, pp. 3755–3777, 1996.
[9] Bottega, W.J. and Loia, M.A., "Axisymmetric edge debonding in patched plate", International Journal of Solids and Structures, Vol. 34, pp. 2255–2289, 1997.
[10] Mohammadi, B., "Repaing of aluminum plates having a crack in mixture mode using ofcomposite patches", MSc Thesis, Amirkabir University of Technology, Department of aerospace engineering, 2002.
[11] Mohammadi, B., "Repaing of aluminum plates having a crack in mixture mode using ofcomposite patches", MSc Thesis, Amirkabir University of Technology, Department of aerospace engineering, 2002.
[12] Sadeghi, G., "3-D Analysis on Damage Tolerance of Repaired Aluminum Panels Using Composite Patches", MSc Thesis, Amirkabir University of Technology, Department of aerospace engineering, 2004.
[13] Bakhshandeh, S., " Experimental investigations on fatigue crack growth of repaired panels with Composite Patches ", MSc Thesis, Amirkabir University of Technology, Department of aerospace engineering, 2004.
[14] Hosseini-Toudeshky, H. Bakhshandeh, S. Mohammadi, B. and Daghyani, H.R., "Experimental investigations on fatigue crack growth of repaired thick aluminum panels in mixed-mode conditions", Composite Structures, Vol. 75, pp.428-436, 2006.
[15] Hosseini-Toudeshky, H. Mohammadi, B. and Daghyani, H.R., "Mixed–mode fracture analysis of repaired aluminum panels using composite patches" Composite Science and Technology, Vol. 66, pp. 188-198, 2006.
[16] Hosseini-Toudeshky, H. Mohammadi, B. and Bakhshandeh, S., "Mixed-mode fatigue crack growth of thin aluminium panels with single-side repair using experimental and numerical methods", Journal of Fatigue & Fracture of Engineering Materials & Structures, Vol. 30, pp. 629-639, 2007.
[17] Hosseini-Toudeshky, H. and Mohammadi, B., "A simple method to calculate the crack growth life of adhesively repaired aluminum panels", Composite Structures, Vol. 79, pp. 234-241, 2007.
[18] Hosseini-Toudeshky, H. Mohammadi, B. Daghyani, H.R. and Sadeghi, G., "Numerical and experimental fatigue crack growth analysis in mode-I for repaired aluminum panels using composite material", Composites: Part A, Vol. 38, pp. 1141-1148, 2007.
[19] Saber, M., "3D crack propagation of cracked thin and thick aluminum panels Repaired with Composite Patches in mixed-mode conditions ", MSc Thesis, Amirkabir University of Technology, Department of aerospace engineering, 2006.
[20] Hosseini-Toudeshky, H. Saber, M. and Mohammadi, B., "Real 3D crack-front and crack trajectory analyses of single-side repaired thick aluminum panels", Journal of Advanced Materials Research, Vols. 47-50, pp. 777-780, 2008.
[21] Hosseini-Toudeshky, H. and Mohammadi, B., "Mixed-Mode Numerical & Experimental Fatigue Crack Growth Analyses of Thick Aluminum Panels Repaired with Composite Patches" J. of Composite Structures, Vol. 91, pp. 1-8, 2009.
[22] Hosseini-Toudeshky, H. Saber, M. and Mohammadi, B., "Crack trajectory analysis of single-side repaired thin panels in mixed-mode conditions using glass/epoxy patches", Computers and Structures, Vol. 86, pp. 997–1005, 2008.
[23] Hosseini-Toudeshky, H. Saber, M. and Mohammadi, B., "Real 3D crack propagation of single-side repaired thin aluminum panels in mixed-mode conditions", International Journal of Fracture, Vol. 153, No. 2, pp. 105-116, 2008.
[24] Hosseini-Toudeshky, H. Saber, M. and Mohammadi, B., "Finite element crack propagation of adhesively bonded repaired panels in general mixed-mode conditions", Finite Elements in Analysis and Design, Vol. 45, pp. 94-103, 2009.
[25] Payganeh, G. H. Ashenai Ghasemi, F. Pourkamali Anaraki, A. and Fallah Rahmatabadi, A., “Numerical analysis for determination of the J integral and crack opening displacement in the cracked aluminum plates repaired with FML composite patches”, Journal of Applied Sciences, Vol. 12, No. 21, pp. 2259–2265, 2012.
[26] Belytschko, T. and Black, T., "Elastic crack growth in finite elements with minimal remeshing.", International Journal for Numerical Methods in Engineering, Vol. 45, pp. 601–620, 1999.
[27] Moes, N. Dolbow, J. and Belytschko, T., "A finite element method for crack growth without remeshing", International Journal for Numerical Methods in Engineering, Vol. 46, pp. 131–150, 1999.
[28] Sukumar, N. Mos, N. and Belytschko, T., "Extended finite element method for three-dimensional crack modelling.", International Journal for Numerical Methods in Engineering, Vol. 76, pp. 1328–1352, 2000.
[29] Moes, N. and Belytschko, T., " Extended finite element method for co
hesive crack growth.", International Journal for Numerical Methods in Engineering, Vol. 69, pp. 813-833, 2002.
[30] Zi, G. and Belytschko, T., " New crack-tip elements for xfem and applications to cohesive cracks.", International Journal for Numerical Methods in Engineering, Vol. 57, pp. 2221-2240, 2003.
[31] de Borst, R. Gutirrez, M. Wells, G. Remmers, J. and Askes, H., "Cohesive-zone models, higher-order continuum theories and reliability methods for computational failure analysis", International Journal for Numerical Methods in Engineering, Vol. 60, pp. 289-315, 2004.
[32] de Borst, R. Remmers, JJ. and Needleman, A., " Mesh-independent discrete numerical representations of cohesive-zone models.", International Journal for Numerical Methods in Engineering, Vol. 73, pp. 160-177, 2006.
[33] Mariani, S. and Perego, U., "xtended finite element method for quasi-brittle fracture.", International Journal for Numerical Methods in Engineering, Vol. 58, pp. 103-126, 2003.
[34] Asferg, J. Poulsen, P. and Nielsen, L., "A consistent partly cracked xfem element for cohesive crack growth.", International Journal for Numerical Methods in Engineering, Vol. 72, pp. 464-485, 2007.
[35] Osher, S. and Sethian, J.A., " Fronts propagating with curvature-dependent speed: Algorithms based on hamilton-jacobi formulations. ", International Journal for Numerical Methods in Engineering, Vol. 79, pp. 12-49, 1988.
[36] Osher, S. and Fedkiw, R., " Level Set Methods and Dynamic Implicit Surfaces", 2003.
[37] Bordas, S., Duflot, M., and Le, P., " A simple error estimator for extended finite elements.", Communications in Numerical Methods in Engineering, Vol. 24, pp. 961-971, 2008.
[38] Chahine, E. Laborde, P. and Renard, Y., " rack tip enrichment in the xfem using a cutoff function.", International Journal for Numerical Methods in Engineering, Vol. 75, pp. 626-646, 2008.
[39] Chahine, E. Laborde, P. and Renard, Y., "quasi-optimal convergence result for fracture mechanics with xfem", International Journal for Numerical Methods in Engineering, Vol. 342. pp. 527-532, 2006.
[40] Lew, A. and shen, Y., " Crack tip enrichment in the xfem using a cut off function", International Journal for Numerical Met.2ds in Engineering, 2009.
[41] Ashenai Ghasemi, F. Pourkamali Anaraki, A. and Rouzbahani, A. H., " Using XFEM for investigating the crack growth of cracked aluminum plates repaired with fiber metal laminate (FML) patches", Journal of Modares Mechanical Engineering, 2012.