A general model of fatigue crack growth under variable amplitude loading

A general model of fatigue crack growth (FCG) in ductile alloys under variable amplitude loading is proposed based on the passivation-lancet theory and the crack closure concept. The model can capture the interactions of single cycle overloading and underloading, sequential loading and spectrum load...

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Bibliographic Details
Published inScience China. Technological sciences Vol. 55; no. 3; pp. 673 - 683
Main Authors Liu, JianTao, Du, PingAn, Zhang, ZhenYu
Format Journal Article
LanguageEnglish
Published Heidelberg SP Science China Press 01.03.2012
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Summary:A general model of fatigue crack growth (FCG) in ductile alloys under variable amplitude loading is proposed based on the passivation-lancet theory and the crack closure concept. The model can capture the interactions of single cycle overloading and underloading, sequential loading and spectrum loading effectively. Moreover, the retardation effect due to overloads and the acceleration effect due to underloading can be described quantitatively by a transition function of crack opening stress. The fa- tigue test data in 2024-T351, 2024-T3 and 7075-T6 aluminum alloys under different types of variable amplitude loading and spectrum loading are used to validate the general model and the predictions by the general model are in good agreement with the test data. Furthermore, the predictions are also compared with the existing models, including FASTRAN, AFGROW and the state-space model, and the comparison results show that the general model predicts the FCG process more accurately.
Bibliography:A general model of fatigue crack growth (FCG) in ductile alloys under variable amplitude loading is proposed based on the passivation-lancet theory and the crack closure concept. The model can capture the interactions of single cycle overloading and underloading, sequential loading and spectrum loading effectively. Moreover, the retardation effect due to overloads and the acceleration effect due to underloading can be described quantitatively by a transition function of crack opening stress. The fa- tigue test data in 2024-T351, 2024-T3 and 7075-T6 aluminum alloys under different types of variable amplitude loading and spectrum loading are used to validate the general model and the predictions by the general model are in good agreement with the test data. Furthermore, the predictions are also compared with the existing models, including FASTRAN, AFGROW and the state-space model, and the comparison results show that the general model predicts the FCG process more accurately.
fatigue and fracture, crack retardation effect, variable loading, crack closure effect, plastic effect
11-5845/TH
ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 23
ISSN:1674-7321
1869-1900
DOI:10.1007/s11431-011-4656-x