[1] Chen, J. F. E. Morozov, V. and Shankar, K., “Simulating Progressive Failure of Composite Laminates Including in-Ply and Delamination Damage Effects,” Composites Part A: Applied Science and Manufacturing, Vol. 61, pp. 185–200 2014.
[2] Maa, R. H. and Cheng, J. H., “A CDM-based Failure Model for Predicting Strength of Notched Composite Laminates,” Composites Part B, Vol. 33, No. 6, pp. 479–489, 2002.
[3] Chen, J. F. Morozov, E. V. and Shankar, K., “A Combined Elastoplastic Damage Model for Progressive Failure Analysis of Composite Materials and Structures,” Compos Struct, Vol. 94, No. 12, pp. 3478–3489, 2012.
[4] Camanho, P. P. Maimí, P. and Dávila, C. G., “Prediction of Size Effects in Notched Laminates Using Continuum Damage Mechanics,” Compos Sci Technol, Vol. 67, No. 13, pp. 2715–2727, 2007.
[5] Farrokhabadi, A. Hosseini-Toudeshky, H. and Mohammadi, B., “Development of a Damage Analysis Method in Laminated Composites Using Finite Fracture Toughness of Single Lamina,” Mech Adv Mat Struc, Vol. 20, pp. 177–188, 2013.
[6] Sadeghi, G. Hosseini-Toudeshky, H. and Mohammadi, B., “An Investigation of Matrix Cracking Damage Evolution in Composite Laminates – Development of an Advanced Numerical Tool,” Composite Structures, Vol. 108, pp. 937–950, 2014.
[7] Lubineau, G. and Ladeveze, P., “Construction of a Micromechanics-based Intralaminar Mesomodel, and Illustrations in ABAQUS/Standard,” Computational Materials Science, Vol 43, No. 17/18, pp. 137-145, 2008.
[8] Shokrieh, M. M. and Ghajar, M., “Simulation of Mode I Strain Energy Release Rate for Laminated Composite Using a Simple Finite Element Model,” In Persian, Majlesi Journal, Vol. 3, No.4, pp. 1-8, 2010.
[9] Torabizadeh, M. A. Shokrieh, M. M. and Fereidoon A., “Progressive Damage Modeling of Glass/Epoxy Laminated Composites under Static Load at Low Temperature,” In Persian, Journal of Modeling in Engineering, Vol. 8, No. 21, pp. 33-43, 2010.
[10] Rybicki, E. F. and Kanninen, M. F., “A Finite Element Calculation of Stress Intensity Factors by a Modified Crack Closure Integral,” Eng Fract Mech, Vol. 9, No. 4, pp. 931–938, 1977.
[11] Ramamurthi, M. and Kim, Y. S., “Delamination Characterization of Bonded Interface Using Surface Based Cohesive Model,” in Supplemental proceeding of TMS 2012 141st Annual Meeting & Exhibition, Volume 1: Materials Processing and Interfaces, John Wiley & Sons, Inc., Hoboken, NJ; pp. 289–296, 2012.
[12] Hallett, S. R. and Wisnom, M. R., “Numerical Investigation of Progressive Damage and the Effect of Layup in Notched Tensile Tests,” J Compos Mater, Vol. 40, No. 14, pp. 1229–1245, 2006.
[13] Camanho, P. P. Dávila, C. G. and de Moura, M. F., “Numerical Simulation of Mixed-mode Progressive Delamination in Composite Materials,” J Compos Mater, Vol. 37, No. 16, pp. 1415–1438, 2003.
[14] Pinho, S. T. Iannucci, L. and Robinson, P., “Formulation and Implementation of Decohesion Elements in an Explicit Finite Element Code,’ Composites Part A, Vol. 37, No. 5, pp. 778–789, 2006.
[15] Borg, R. Nilsson, L. and Simonsson, K., “Simulation of Delamination in Fiber Composites with a Discrete Cohesive Failure Model,” Compos Sci Technol, Vol. 61, No. 5, pp. 667–677, 2001.
[16] Tserpes, K. I. Papanikos, P. and Kermanidis, T., “A Three-dimensional Progressive Damage Model for Bolted Joints in Composite Laminates Subjected to Tensile Loading,” Fatigue Fract Engng Mater Struct, Vol. 24, No. 10, pp. 663–675, 2001.
[17] Atas, A. Mohamed, G. F. and Soutis, C., “Modeling Delamination Onset and Growth in Pin Loaded Composite Laminates,” Compos Sci Technol, Vol. 72, No. 10, pp. 1096–1101, 2012.
[18] Daudeville, L. Allix, O. and Ladeveze, P., “Delamination Analysis by Damage Mechanics: Some Applications,” Compos Eng, Vol. 5, No. 1, pp. 17–24, 1995.
[19] Alfano, G., “On the Influence of the Shape of the Interface Law on the Application of Cohesive-zone Models,” Composites Science and Technology, Vol. 66, pp. 723–730, 2006.
[20] de Morais, A. B. and Pereira, A. B., “Application of the Effective Crack Method to Mode I and Mode II Interlaminar Fracture of Carbon/Epoxy Unidirectional Laminates,” Composites: Part A, Vol. 38, pp. 785–794, 2007.
[21] Shokrieh, M. M. Salamat-Talab, M. and Heidari-Rarani, M., “Numerical Analysis of Mode I Delamination Growth in Laminated DCB Specimens Using Cohesive Zone Models,” In Persian, Modares Mechanical Engineering, Vol. 13, No. 1, pp. 38-48, 2013.
[22] Heidari-Rarani, M. Shokrieh, M. M. and Camanho, P. P., “Finite Element Modeling of Mode I Delamination Growth in Laminated DCB Specimens with R-curve Effects,” Composites: Part B, Vol. 45, pp. 897–903, 2013.
[23] Shokrieh, M. M. and Zeinedini, A., “Prediction of Strain Energy Release Rate of Asymmetric Double Cantilever Composite Beam in Mixed-mode I/II Delamination using Equivalent Lay-up,” In Persian, Modares Mechanical Engineering, Vol. 13, No. 13, pp. 214-225, 2014.
[24] Saeedifar, M. Fotouhi, M. Mohammadi, R. Ahmadi Najafabadi, M. and Hosseini Toudeshky, H., “Investigation of Delamination and Interlaminar Fracture Toughness Assessment of Glass/Epoxy Composite by Acoustic Emission,” In Persian, Modares Mechanical Engineering, Vol. 14, NO. 4, pp. 1-11, 2014.
[25] Abaqus Analysis User’s Manual, Version 6.12-1, Dassault Systèmes Simulia Corp., Providence, RI.
[26] Hashin, Z., “Failure Criteria for Unidirectional Fiber Composites,” Journal of Applied Mechanics, Vol. 47, pp. 329–334, 1980.
[27] Naghipour, P. Bartsch, M. Chernova, L. Hausmann, J. and Voggenreiter, H., “Effect of Fiber Angle Orientation and Stacking Sequence on Mixed Mode Fracture Toughness of Carbon Fiber Reinforced Plastics: Numerical and Experimental Investigations,” Mater. Sci. Eng. A, Vol. 527, No. 3, pp. 509–517, 2010.
[28] Pinho, S. T. Robinson, P. and Iannucci, L., “Fracture Toughness of the Tensile and Compressive Fibre Failure Modes in Laminated Composites,” Compos. Sci. Technol., Vol. 66, No. 13, pp. 2069–2079, 2006.
[29] Pinho, S. T., “Modelling Failure of Laminated Composites Using Physi- cally-based Failure Models,” PhD thesis. Department of Aeronautics, Imperial College London, UK, 2005
[30] Chai, H., “Interlaminar Shear Fracture of Laminated Composites,” Int J Fracture, Vol. 43, No. 2, pp. 117–131, 1990.
[31] Wisnom, M. R. Khan, B. and Hallett, S. R., “Size Effects in Unnotched Tensile Strength of Unidirectional and Quasi-isotropic Carbon/Epoxy Composites,” Compos Struct, Vol. 84, No. 1, pp. 21–28, 2008.{Carey, 1998 #8}