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dc.creatorPavlou, D. G.en
dc.creatorVlachakis, N. V.en
dc.creatorPavlou, M. G.en
dc.creatorVlachakis, V. N.en
dc.date.accessioned2015-11-23T10:45:16Z
dc.date.available2015-11-23T10:45:16Z
dc.date.issued2004
dc.identifier10.1016/j.commatsci.2003.12.003
dc.identifier.issn0927-0256
dc.identifier.urihttp://hdl.handle.net/11615/32115
dc.description.abstractQuantitative analysis is provided to estimate the reduction of fatigue crack growth rate due to overload crack branching. A recent mixed-mode fatigue crack growth model based on the dilatational component of the accumulated strain energy density near the crack tip is modified to quantify the retardation factor of crack growth rate following an overload. It is found that crack branching due to an overload results in considerable reduction of fatigue crack growth rate. The retardation factor estimated by the proposed methodology is correlated with test results for the 2090-T8E41 aluminum-lithium alloy indicating encouraging agreement. (C) 2003 Elsevier B.V. All rights reserved.en
dc.source.uri<Go to ISI>://WOS:000220633900007
dc.subjectcrack growthen
dc.subjectretardationen
dc.subjectcrack branchingen
dc.subjectfatigueen
dc.subjectPREDICTIONen
dc.subjectMECHANISMSen
dc.subjectOVERLOADSen
dc.subjectMaterials Science, Multidisciplinaryen
dc.titleEstimation of fatigue crack growth retardation due to crack branchingen
dc.typejournalArticleen


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