2021
DOI: 10.1016/j.engfracmech.2021.108087
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Development of higher-order displacement discontinuity method to simulate fatigue crack growth in brittle materials

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Cited by 15 publications
(12 citation statements)
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“…In the framework of the scheme followed by the proposed strategy to estimate the fatigue life, both the crack tips advance simultaneously along the propagation directions determined by Equation (17), and, at crack increments of 0.5 mm, the number of cycles (ΔN) for both the tips is evaluated using Paris' law. Figure 15A compares the propagation paths predicted by the proposed method and those achieved experimentally by Pustejovsky 16 and numerically by Saijth et al, 24 Alizadeh et al, 31 and de Castro e Andrade and Leonel. 69 The figure also reports the snapshots of the computational mesh corresponding to the position occupied by crack tips marked by Roman numerals in the graph, which provides an exhaustive overview of how the mesh evolves during the numerical simulation.…”
Section: Case 2: Fatigue Life Estimation Of a Holed Platementioning
confidence: 86%
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“…In the framework of the scheme followed by the proposed strategy to estimate the fatigue life, both the crack tips advance simultaneously along the propagation directions determined by Equation (17), and, at crack increments of 0.5 mm, the number of cycles (ΔN) for both the tips is evaluated using Paris' law. Figure 15A compares the propagation paths predicted by the proposed method and those achieved experimentally by Pustejovsky 16 and numerically by Saijth et al, 24 Alizadeh et al, 31 and de Castro e Andrade and Leonel. 69 The figure also reports the snapshots of the computational mesh corresponding to the position occupied by crack tips marked by Roman numerals in the graph, which provides an exhaustive overview of how the mesh evolves during the numerical simulation.…”
Section: Case 2: Fatigue Life Estimation Of a Holed Platementioning
confidence: 86%
“…The fatigue behavior of a titanium plate containing an internal oblique crack. A comparison between the proposed method and the results achieved experimentally by Pustejovsky 16 and numerically by Saijth et al, 24 Alizadeh et al, 31 achieved experimentally by Pustejovsky 16 and numerically by other numerical methodologies. 24,31,69 In this context, the best fit occurs with the results of Sajith et al, 24 which report a fatigue life smaller than that predicted by the proposed method of 1.47%.…”
Section: Case 2: Fatigue Life Estimation Of a Holed Platementioning
confidence: 88%
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