Issue 50

F. Larbi Chaht et alii, Frattura ed Integrità Strutturale, 50 (2019) 331-341; DOI: 10.3221/IGF-ESIS.50.28 341 [13] Guo ,Y . ( 2000).Eight-Node Solid Element for Thick Shell Simulations, Livermore Software Technology Corporation Livermore, California, USA, 8, pp. 46. [14] Barberon, E., Shahbazi, M .(2017). Determination of Material Properties for ANSYS Progressive Damage Analysis of Laminated Composites. Composite Structures, 176, pp. 768–779. [15] Davila,C G., Camanho, P P., Rose, C A .(2005). Failure Criteria for FRP Laminates. Journal of composite materials. DOI: 10.1177 /0021998305046452 . [16] ABAQUS finite element programs. ABAQUS iStandard 5.6. Hibbitt. Pawtucket, RI 028: Karlsson and Sorensen, Inc. [17] Sokolinsky, V. (2013). Using Failure Criteria for Unidirectional Fiber Composite in Abaqus, Simulia. [18] Pederson, J. (2006).Finite Element Analysis of Carbon Composite Ripping using Abaqus. Masters diss, Clesmo University. Available at: https://tigerprints.clemson.edu/cgi/viewcontent.cgi?article=1512&context=all_theses. [19] Computer Aided Design Environment for Composites, CADEC 14.1.6521.18183. Available at: http://en.cadec-online.com/. [20] Trigo, J.(1996). Dimentional stability characterization of carbon fiber with epoxy and cyanate ester resin laminates due to moisture Absorption.Space craft structures. materials and mechanical engineering, Proceedings of the Conference held by ESA, CNES and DARA in Noordwijk, Paris.