Issue 50

Frattura ed Integrità Strutturale, 50 (2019); International Journal of the Italian Group of Fracture I Table of Contents O. Plekhov, A. Vshivkov The effect of fatigue crack rate on the heat dissipation in metals under mixed-mode loading …...... 1-8 M.F. Borges, F.V. Antunes, P. Prates, R. Branco, M.C. Oliveira Effect of yield stress on fatigue crack growth ………………………………………….... 9-19 Z.-y. Han, X.-g. Huang Stress corrosion behavior of X80 pipeline steel in the natural seawater with different dissolved oxygen contents ……………………………………………………………………. 20-28 G. Khandouzi, M. Mollashahi, M. Moosakhani Numerical simulation of crack propagation behavior of a semi-cylindrical specimen under dynamic loading ……….....................................................................................................………... 29-37 M. Eremin, A. Kulkov, I. Smolin, V. Mikushina Investigation of Failure Mechanism of Al 2 O 3 Specimens Subjected to Three-Point Bending Test 38-45 I. G. F. da Silva, A. H. P. de Andrade, W. A. Monteiro Leak-Before-Break methodology applied to different piping materials: a performance evaluation 46-53 N. Boychenko, I. Ishtyryakov Characterization of the stress-strain state in a gas turbine engine compressor disc taking into account damage accumulation ………..………………………………………………. 54-67 M. Baghdadi, B. Serier, M. Salem, B. Zaoui, K. Kaddouri Modeling of a cracked and repaired Al 2024T3 aircraft plate: effect of the composite patch shape on the repair performance. …………………………………...……………………..... 68-85 A. Sarkar, A. Nagesha, R. Sandhya, M. Okazaki Crack growth based life prediction approach under LCF-HCF interaction ………………..... 86-97 R. Boutelidja, A. Guedri, M. A. Belyamna, B. Merzoug Environmental effects on the reliability of an AISI 304 structure …………………………. 98-111 B. Benamar, M. Mokhtari, K. Madani, H. Banzaama Using a cohesive zone modeling to predict the compressive and tensile behavior on the failure load of single lap bonded joint ………………………… …………………..…………………… 112-125 O. Mouhat, A. Bybi, A. El Bouhmidi, M. Rougui Effects of ply orientation on nonlinear buckling of aircraft composite stiffened panel ...………… 126-140