1-
[1] Liu, P., Xu, P., Zheng, J., “Artificial immune system for optimal design of composite hydrogen storage vessel“, Computational Materials Science, Vol. 47, No. 1, pp. 261-267, 2009.
[2] Zheng, J., Liu, P., “Elasto-plastic stress analysis and burst strength evaluation of Al-carbon fiber/epoxy composite cylindrical laminates“, Computational Materials Science, Vol. 42, No. 3, pp. 453-461, 2008.
[3] Mohammadi, B. Fazlali, B., “Fatigue life prediction of laminated composites under multiaxial fatigue loading condition by using developed continuum damage mechanics model”, In Persian, Journal of Science and Technology of Composites, Vol. 3, No. 3, pp. 215-224, 2016.
[4] Lapczyk, I., Hurtado, J. A., “Progressive damage modeling in fiber-reinforced materials“, Composites Part A: Applied Science and Manufacturing, Vol. 38, No. 11, pp. 2333-2341, 2007.
[5] Shokrieh, M. M. Ghajar, M. Salamattalab, M. and Madoliat, R., “Progressive damage modeling of laminated composites by considering simultaneous effects of interlaminar and intralaminar damage mechanisms”, In Persian, Journal of Science and Technology of Composites, Vol. 2, No. 2, pp. 1-8, 2015.
[6] Pietropaoli, E., “Progressive Failure Analysis of Composite Structures Using a Constitutive Material Model (USERMAT) Developed and Implemented in ANSYS©“, Applied Composite Materials, Vol. 19, No. 3-4, pp. 657-668, 2012.
[7] Bouazza, M., Tounsi, A., Benzair, A., Adda-Bedia, E., “Effect of transverse cracking on stiffness reduction of hygrothermal aged cross-ply laminates“, Materials & design, Vol. 28, No. 4, pp. 1116-1123, 2007.
[8] Spottswood, S. M., Palazotto, A. N., “Progressive failure analysis of a composite shell“, Composite structures, Vol. 53, No. 1, pp. 117-131, 2001.
[9] 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.
[10] Kachanov, L., “Time of the rupture process under creep conditions“, Isv. Akad. Nauk. SSR. Otd Tekh. Nauk, Vol. 8, pp. 26-31, 1958.
[11] Hashin, Z., Rotem, A., “A fatigue failure criterion for fiber reinforced materials“, Journal of composite materials, Vol. 7, No. 4, pp. 448-464, 1973.
[12] Czichon, S., Zimmermann, K., Middendorf, P., Vogler, M., Rolfes, R., “Three-dimensional stress and progressive failure analysis of ultra thick laminates and experimental validation“, Composite Structures, Vol. 93, No. 5, pp. 1394-1403, 2011.
[13] Camanho, P., Arteiro, A., Melro, A., Catalanotti, G., Vogler, M., “Three-dimensional invariant-based failure criteria for fibre-reinforced composites“, International Journal of Solids and Structures, Vol. 55, pp. 92-107, 2015.
[14] Matzenmiller, A., Lubliner, J., Taylor, R., “A constitutive model for anisotropic damage in fiber-composites“, Mechanics of materials, Vol. 20, No. 2, pp. 125-152, 1995.
[15] Vo, T., Guan, Z., Cantwell, W., Schleyer, G., “Low-impulse blast behaviour of fibre-metal lami“, Composite Structures, Vol. 94, No. 3, pp. 954-965, 2012.
[16] Hibbitt, H., Karlsson, B., Sorensen, P., “ABAQUS theory manual, version 6.3“, Pawtucket, Rhode Island, USA, 2006.
[17] Puck, A., Schürmann, H., “Failure analysis of FRP laminates by means of physically based phenomenological models“, Composites Science and Technology, Vol. 58, No. 7, pp. 1045-1067, 1998.
[18] Liu, P., Zheng, J., “Recent developments on damage modeling and finite element analysis for composite laminates: a review“, Materials & Design, Vol. 31, No. 8, pp. 3825-3834, 2010.
[19] Tsai, S. W., Wu, E. M., “A general theory of strength for anisotropic materials“, Journal of composite materials, Vol. 5, No. 1, pp. 58-80, 1971.
[20] Hoffman, O., “The brittle strength of orthotropic materials“, Journal of Composite Materials, Vol. 1, No. 2, pp. 200-206, 1967.
[21] Yamada, S., Sun, C., “Analysis of laminate strength and its distribution“, Journal of Composite Materials, Vol. 12, No. 3, pp. 275-284, 1978.
[22] Spencer, A., “Kinematic constraints, constitutive equations and failure rules for anisotropic materials“, in: Applications of Tensor Functions in Solid Mechanics, Eds., pp. 187-201: Springer, 1987.
[23] Camanho, P. P., Dávila, C. G., “Mixed-mode decohesion finite elements for the simulation of delamination in composite materials“, NASA, pp. 1–37, 2002.
[24] Mohammadi, B. Kazemi, A. and Ghasemi, R., “Damage analysis of holed composite laminates using continuum damage mechanics”, In Persian, Journal of Science and Technology of Composites, Vol. 2, No. 3, pp. 23-34, 2015.
[25] Suemasu, H., Takahashi, H., Ishikawa, T., “On failure mechanisms of composite laminates with an open hole subjected to compressive load“, Composites Science and Technology, Vol. 66, No. 5, pp. 634-641, 2006.
[26] Kottner, R., Hynek, R., Kroupa, T., “Identification of parameters of cohesive elements for modeling of adhesively bonded joints of epoxy composites“, Applied and Computational Mechanics, Vol. 7, No. 2, 2013.
[27] El-Sisi, A. E.-D. A., El-Emam, H. M., Salim, H. A., Sallam, H. E.-D. M., “Efficient 3D modeling of damage in composite materials“, Journal of Composite Materials, pp. 0021998314525983, 2014.
[28] Eng, C. H., “Compressive Failure of Open-Hole Carbon Composite Laminates“, MSc Thesis, Department of Mechanical Engineering, National University of Singapore, Singapore, 2007.