Issue 49

M. Tashkinov et alii, Frattura ed Integrità Strutturale, 49 (2019) 396-411; DOI: 10.3221/IGF-ESIS.49.39 411 [28] Gotsis, P.K., Chamis, C.C., Minnetyan, L. (2004).Prediction of composite laminate fracture: Micromechanics and progressive fracture. Failure Criteria in Fibre-Reinforced-Polymer Composites. [29] Garnich, M.R., Akula, V.M.K. (2008). Review of Degradation Models for Progressive Failure Analysis of Fiber Reinforced Polymer Composites, Appl. Mech. Rev., DOI: 10.1115/1.3013822. [30] Wang, C., Roy, A., Silberschmidt, V. V., Chen, Z. (2017). Modelling of Damage Evolution in Braided Composites: Recent Developments, Mech. Adv. Mater. Mod. Process., 3(1), pp. 15, DOI: 10.1186/s40759-017-0030-4. [31] Ullah, H., Harland, A.R., Silberschmidt, V. V. (2012). Damage modelling in woven-fabric CFRP laminates under large-deflection bending, Comput. Mater. Sci., 64, pp. 130–135, DOI: 10.1016/j.commatsci.2012.05.036. [32] Tomblin, J., Sherraden, J., Seneviratne, W., Raju, K.S. (2002). A-Basis and B-Basis Design Allowables for Epoxy- based Prepreg Toray T700GC-12K-31E/#2510 Unidirectional Tape (SI Units), . [33] Mori, T., Tanaka, K. (1973). Average stress in matrix and average elastic energy of materials with misfitting inclusions, Acta Metall., 21(5), pp. 571–574, DOI: 10.1016/0001-6160(73)90064-3. [34] Ivanov, D.S., Lomov, S. V. (2014). Modelling the structure and behaviour of 2D and 3D woven composites used in aerospace applications, Elsevier Ltd.