2001
DOI: 10.1016/s0307-904x(01)00027-0
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Fatigue crack growth under variable-amplitude loading: Part II – Code development and model validation

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Cited by 66 publications
(43 citation statements)
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“…The changes of a stress ratio related to changing of minimum stress with a constant maximum stress. The data predicted using the Austen, modified Forman and NASGRO models are compared with those models performed by previous literatures [Ray & Patanker, 2001b;Huang, et al, 2005a;Huang, et al, 2005b]. The maximum differences in life predicting for the load cases for all models are 40% as a maximum compared to the test data.…”
Section: Resultsmentioning
confidence: 93%
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“…The changes of a stress ratio related to changing of minimum stress with a constant maximum stress. The data predicted using the Austen, modified Forman and NASGRO models are compared with those models performed by previous literatures [Ray & Patanker, 2001b;Huang, et al, 2005a;Huang, et al, 2005b]. The maximum differences in life predicting for the load cases for all models are 40% as a maximum compared to the test data.…”
Section: Resultsmentioning
confidence: 93%
“…Thus, the fatigue crack propagation models under VA loading are presented in this section based on the Austen, modified Forman and NASGRO models. For demonstrating the validation of these models predictions are compared with test data, FASTRN and AFGROW codes given in Ray and Patanker [2001b].…”
Section: Resultsmentioning
confidence: 99%
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“…In contrast, the crack growth caused by variable amplitude loading is characterized by acceleration and retardation effects [1][2][3], which significantly affect the RUL. Currently there are many physics based models [1][2][3][4][5][6] to model crack growth with acceleration and retardation effects. These models capture the fatigue crack growth phenomena reasonably well under variable loading, but in a deterministic framework.…”
Section: Introductionmentioning
confidence: 99%