2018
DOI: 10.1155/2018/4048386
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Application of a Cohesive Zone Model for Simulating Fatigue Crack Growth from Moderate to High ΔK Levels of Inconel 718

Abstract: A cyclic cohesive zone model is applied to characterize the fatigue crack growth behavior of a IN718 superalloy which is frequently used in aerospace components. In order to improve the limitation of fracture mechanics-based models, besides the predictions of the moderate fatigue crack growth rates at the Paris' regime and the high fatigue crack growth rates at the high stress intensity factor ΔK levels, the present work is also aimed at simulating the material damage uniformly and examining the influence of t… Show more

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Cited by 5 publications
(3 citation statements)
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References 30 publications
(52 reference statements)
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“…Metals 2024, 14, x FOR PEER REVIEW 9 of 37 logarithmic coordinates, Paris' law (Equation ( 7)) establishes a connection between the stress intensity factor range (ΔK) and the crack growth rate (da/dN). The alterations made to Paris' law for determining crack growth rates proved highly effective in enhancing the accuracy of fatigue life predictions in engineering design [47].…”
Section: Fatigue Crack Growth Rate (Fcgr)mentioning
confidence: 99%
See 1 more Smart Citation
“…Metals 2024, 14, x FOR PEER REVIEW 9 of 37 logarithmic coordinates, Paris' law (Equation ( 7)) establishes a connection between the stress intensity factor range (ΔK) and the crack growth rate (da/dN). The alterations made to Paris' law for determining crack growth rates proved highly effective in enhancing the accuracy of fatigue life predictions in engineering design [47].…”
Section: Fatigue Crack Growth Rate (Fcgr)mentioning
confidence: 99%
“…The stress intensity factor curve for metallic materials typically exhibits three distinct regimes when it comes to fatigue crack growth rate. Reprinted from ref [47]…”
mentioning
confidence: 99%
“…The cohesive element type was the 2D 4-node cohesive element COH2D4. Literature [16,20,[35][36][37] suggests that the plane strain assumption should be used when specimen thickness is in the range of 9-12.5 mm. Literature [12,38] argues that when the CT specimen thickness is in the range of 3-5 mm, the plane stress assumption should be used.…”
Section: Development Of Finite Element Modelsmentioning
confidence: 99%