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[1] Martin Alberto MASUELLI, Fiber Reinforced Polymers - The Technology  Applied for Concrete Repair . InTech, 2013.  [2] F. A. Administration, Aviation Maintenance Technician Handbook    Airframe:  FAA-H-8083-31 Volume 1 , 2012 Edition edition. Newcastle, Wash.: Aviation Supplies and Academics, Inc., 2012.  [3] P. P. Camanho, P. Maimí, and C. G. Dávila, Prediction of size effects in notched laminates using continuum damage mechanics,Composites Science and Technology, vol. 67, no. 13, pp. 2715   2727, Oct. 2007.  [4] M. J. Hinton and P. D. Soden, Predicting failure in composite laminates: the  background to the exercise,Composites Science and Technology , vol. 58, no. 7,  pp. 1001   1010, Jul. 1998.  [5] M. J. Hinton and A. S. Kaddour, The background to Part B of the Second World - Wide Failure Exercise: Evaluation of theories for predicting failure in pol ymer composite laminates under three- dimensional states of stress, Journal of Composite Materials, p. 0021998312473346, Jan. 2013.  [6] J. M. Whitney and R. J. Nuismer, Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations, Journal of Composite Materials , vol. 8, no. 3, pp. 253   265, Jul. 1974.  [7] Karlak, R.F. Hole effects in a related series of s ymmetrical laminates. In Proceedings of the Conference on Failure Modes in Composite (IV), Chicago, IL, USA, 1   3 January 1977. [8] Pipes, R.B.; Wetherhold, R.C.; Gillespie, J.W. Notched strength of composite - materials. J. Composit. Mater. 1979, 13, 148   160. [9] Echaabi, J.; Trochu, F.; Gauvin, R. Review of failure criteria of fibrous composite materials. Polym. Composit. 1996, 17 , 786   798. [10] Chamis, C.C. Polymer composite mechanics review   1965 to 2006.  J. Reinf.  Plast. Composit. 2007, 26 , 987   1019. [11] Hashin, Z. Failure criteria for unidirectional fiber composites.  J. Appl. Mech. Trans. Asme 1980, 47 , 329   334. [12] Puck, A. A failure criterion shows the direction. Kunststoffe-German Plast. 1992, 82, 607   610. [13] Chang, F.K.; Chang, K.Y. A progressive damage model for laminated composites containing stress-concentrations. J. Composit. Mater. 1987, 21, 834   855. [14] Chang, F.K.; Lessard, L.B. Damage tolerance of laminated composites containing an open hole and subjected to compressive loadings: 1. Analysis.  J. Composit.  Mater. 1991, 25, 2   43. [15] Tan, S.C. A progressive failure model for composite laminates co ntaining openings. J. Composit. Mater. 1991, 25, 556   577. [16] Tan, S.C.; Perez, J. P rogressive failure of laminated composites with a hole under compressive loading.  J. Reinf. Plast. Composit. 1993, 12, 1043   1057. [17] Camanho, P.P.; Matthews, F.L. A p rogressive damage model for mechanically fastened joints in composite laminates.  J. Composit. Mater. 1999, 33, 2248   2280. 

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[1] Martin Alberto MASUELLI, Fiber Reinforced Polymers - The Technology Applied for Concrete Repair. InTech, 2013.[2] F. A. Administration, Aviation Maintenance Technician HandbookAirframe: FAA-H-8083-31 Volume 1, 2012 Edition edition. Newcastle, Wash.: Aviation Supplies and Academics, Inc., 2012.[3] P. P. Camanho, P. Maim, and C. G. Dvila, Prediction of size effects in notched laminates using continuum damage mechanics, Composites Science and Technology, vol. 67, no. 13, pp. 27152727, Oct. 2007.[4] M. J. Hinton and P. D. Soden, Predicting failure in composite laminates: the background to the exercise, Composites Science and Technology, vol. 58, no. 7, pp. 10011010, Jul. 1998.[5] M. J. Hinton and A. S. Kaddour, The background to Part B of the Second World-Wide Failure Exercise: Evaluation of theories for predicting failure in polymer composite laminates under three-dimensional states of stress, Journal of Composite Materials, p. 0021998312473346, Jan. 2013.[6] J. M. Whitney and R. J. Nuismer, Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations, Journal of Composite Materials, vol. 8, no. 3, pp. 253265, Jul. 1974.[7] Karlak, R.F. Hole effects in a related series of symmetrical laminates. In Proceedings of the Conference on Failure Modes in Composite (IV), Chicago, IL, USA, 13 January 1977. [8] Pipes, R.B.; Wetherhold, R.C.; Gillespie, J.W. Notched strength of composite-materials. J. Composit. Mater. 1979, 13, 148160.[9] Echaabi, J.; Trochu, F.; Gauvin, R. Review of failure criteria of fibrous composite materials. Polym. Composit. 1996, 17, 786798.[10] Chamis, C.C. Polymer composite mechanics review1965 to 2006. J. Reinf. Plast. Composit. 2007, 26, 9871019.[11] Hashin, Z. Failure criteria for unidirectional fiber composites. J. Appl. Mech. Trans. Asme 1980, 47, 329334.[12] Puck, A. A failure criterion shows the direction. Kunststoffe-German Plast. 1992, 82, 607610.[13] Chang, F.K.; Chang, K.Y. A progressive damage model for laminated composites containing stress-concentrations. J. Composit. Mater. 1987, 21, 834855.[14] Chang, F.K.; Lessard, L.B. Damage tolerance of laminated composites containing an open hole and subjected to compressive loadings: 1. Analysis. J. Composit. Mater. 1991, 25, 243.[15] Tan, S.C. A progressive failure model for composite laminates containing openings. J. Composit. Mater. 1991, 25, 556577.[16] Tan, S.C.; Perez, J. Progressive failure of laminated composites with a hole under compressive loading. J. Reinf. Plast. Composit. 1993, 12, 10431057.[17] Camanho, P.P.; Matthews, F.L. A progressive damage model for mechanically fastened joints in composite laminates. J. Composit. Mater. 1999, 33, 22482280.[18] Shokrieh, M.M.; Lessard, L.B. Progressive fatigue damage modeling of composite materials, part i: Modeling. J. Composit. Mater. 2000, 34, 10561080.[19] Shokrieh, M.M.; Lessard, L.B. 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