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dc.contributor.authorPapuga, Jan
dc.contributor.authorHalama, Radim
dc.date.accessioned2019-05-28T11:09:23Z
dc.date.available2019-05-28T11:09:23Z
dc.date.issued2019
dc.identifier.citationArchive of Applied Mechanics. 2019, vol. 89, issue 5, special issue, p. 823-834.cs
dc.identifier.issn0939-1533
dc.identifier.issn1432-0681
dc.identifier.urihttp://hdl.handle.net/10084/135095
dc.description.abstractThe paper deals with evaluating the mean stress effect in multiaxial criteria for fatigue limit estimation, with special emphasis on the mean shear stress effect. The usual practice of accepting the mean normal stress effect and neglecting the effect of static torsion is scrutinized. Two methodstwo critical plane criteria, PCr (Papuga Criterion) and QCP (Quadratic parameter on the Critical Plane)are described, and additional local stress parameters representing the mean torsion effect are implemented. The efficiency of the new implementations is evaluated on a large data set of 407 fatigue limits. Additionally, outputs of two other well-known methodsthe Crossland method and the Dang Van methodare provided for comparison. The positive outcome of including the mean shear stress effect is evident not only in cases of applied mean torsion load, but also in cases with purely axial loading or with biaxial configurations.cs
dc.language.isoencs
dc.publisherSpringercs
dc.relation.ispartofseriesArchive of Applied Mechanicscs
dc.relation.urihttps://doi.org/10.1007/s00419-018-1421-7cs
dc.rights© Springer-Verlag GmbH Germany, part of Springer Nature 2018cs
dc.subjectmean stress effectcs
dc.subjectmean torsion loadcs
dc.subjectmultiaxial loadingcs
dc.subjectcritical plane criteriacs
dc.subjectfatigue of materialscs
dc.titleMean stress effect in multiaxial fatigue limit criteriacs
dc.typearticlecs
dc.identifier.doi10.1007/s00419-018-1421-7
dc.type.statusPeer-reviewedcs
dc.description.sourceWeb of Sciencecs
dc.description.volume89cs
dc.description.issue5cs
dc.description.lastpage834cs
dc.description.firstpage823cs
dc.identifier.wos000466859300005


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