PSI - Issue 28

Carlos D.S. Souto et al. / Procedia Structural Integrity 28 (2020) 146–154

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Carlos D.S. Souto et al. / Structural Integrity Procedia 00 (2020) 000–000

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Tavares, S. M. O., de Castro, P. M. S. T., 2019. Damage tolerance of metallic aircraft structures: materials and numerical modelling. SpringerBriefs in Computational Mechanics. Tavares, S. M. O., de Castro, P. M. S. T., 2011. Stress intensity factor calibration for a longitudinal crack in a fuselage barrel and the bulging e ff ect influence. Eng. Fract. Mech., 78(17), pp. 2907-2918. Krueger, R., 2004. Virtual crack closure technique: History, approach, and applications. Appl. Mech. Rev., vol. 57, no. 2, pp. 109-143. Rice, J., 1968. A path independent integral and the approximate analysis of strain concentration by notches and cracks. J. Appl. Mech., 35(2): 379-386. Owen, D., Fawkes, A., 1983. Engineering fracture mechanics: Numerical methods and applications. Pineridge Press Ltd., 1st ed., pp. 45-47. Kuna, M., 2013. Finite elements in fracture mechanics. Springer, Solid Mechanics and Its Applications, vol. 201, pp. 240-243. Abaqus Documentation, 2017. J-Integral Evaluation. https: // abaqus-docs.mit.edu / 2017 / English / SIMACAETHERefMap / simathe-c-jintegral.htm Monteiro, J., 1984. Determinac¸a˜o de fatores de intensidade de tensa˜o usando o me´todo dos elementos finitos. MSc Thesis, Faculty of Engineering of the University of Porto, pp 89-90. Omicron, 2019. Finite Element Analysis Software by Carlos Souto https: // sites.google.com / view / omicron-fea / home