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In this study, fatigue crack growth of edge crack in plate made from 5083 aluminum alloy under mixed mode fracture was numerically investigated. Effect of various parameters include initial crack direction angle (30°, 60°, 90°), initial crack length (20 and 25 mm) and load ratio (R=0 and 0.25) were considered. We also consider the effect of point compression load on crack growth life with 20 mm initial crack length under 30°, 60°, 90° at various parts of crack growth path. Mentioned models were simulated using the finite element softwares, ABAQUS and FRANC2D and their results were compared together. For validation we compare the numerical results for a specimen with its experimental data. Numerical results show good agreement with the experimental data for fracture path. It is observed that the point compression load can affect the path and life of crack growth in fatigue loading. If this load was applied in the first cycles of crack growth, its effect is more than another cases. For instance in the crack growth with initial angle 30o applying point load in 5, 10 and 15 mm of crack growth length, increase the life 79.4%, 18.9% and 6.2% respectively.
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This work compares the fatigue crack growth under constant amplitude load between two softwares, ANSYS Mechanical R19.2 and FRANC2D/L, as an alternative tool for modeling fatigue crack growth problems in mixed-mode loads. Four different configurations of the modified compact tension were simulated in both softwares. The crack growth trajectory, SIFs, stresses distribution, and fatigue life cycles were predicted using both softwares, and the outcome from other researchers validated the results.
Fatigue assessment of materials can be mostly illustrated by three approaches: the fracture mechanics method proposed by Paris and Erdogan [37], the method of strain-life independently obtained by Coffin [38], and the stress-life method proposed by Wöhler [39]. The first method was employed (in the present work) in estimating fatigue life, and the crack tip was characterized independently by the SIFs. 2b1af7f3a8