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Numerical study of in-plane biaxial fatigue crack growth with different phase shift angle loadings on optimal specimen geometries

dc.contributor.authorBaptista, R.
dc.contributor.authorCláudio, R. A.
dc.contributor.authorReis, L.
dc.contributor.authorMadeira, JFA
dc.contributor.authorFreitas, M.
dc.date.accessioned2017-04-05T13:21:08Z
dc.date.available2017-04-05T13:21:08Z
dc.date.issued2016
dc.description.abstractNowadays for real world applications, mechanical components in the automotive, aerospace, aeronautical and other industries are subjected to multiaxial loading conditions. Although the fatigue behavior of materials like steel alloys, aluminum alloys or even magnesium alloys is fairly well established for uniaxial loading, one should not use this knowledge for biaxial loading. Developing new testing machines and new specimen geometries have been the previous goal of several authors. A new generation of smaller and more efficient biaxial fatigue testing machines has arrived on the market. Using electrical motors these machines are not able to achieve the higher loads as their hydraulic counterparts can, and therefore the cruciform specimen needs to be optimized. The authors have previously optimized the cruciform geometry for biaxial fatigue initiation, using a revolved spline to reduce the specimen center thickness. For crack initiation experimental results have proven that the obtained design detail is effective, but there are no studies about the behavior of these specimens for crack propagation. In this paper the authors firstly set out to determine the conditions for crack initiation using traditional criteria like Findley, Brown-Miller, Fatemi-Socie, Smith, Watson and Topper (SWT), Liu I and Chu, as a function of different biaxial loading with phase differences. On a second stage the authors compared the biaxial fatigue crack propagation on the optimal specimens, with the behavior of notched specimens, using the stress intensity factors for mode I and mode II. Several crack and loading parameters were studied, including the starting crack length and angle, and different loading paths. Different biaxial loadings were applied to the model, including 30°, 45°, 60°, 90° and 180° out-of-phase angles. Very similar small crack propagation parameters were obtained for both specimens, although as the crack growths the stress intensity factor for the optimal specimen do not behave as expected. Therefore limiting the use of this specimen for crack propagation.pt_PT
dc.description.versioninfo:eu-repo/semantics/publishedVersionpt_PT
dc.identifier.citationBAPTISTA, R.; [et al] – Numerical study of in-plane biaxial fatigue crack growth with different phase shift angle loadings on optimal specimen geometries. Theoretical and Applied Fracture Mechanics. ISSN 0167-8442. Vol. 85, Part A (2016), pp. 16-25pt_PT
dc.identifier.doihttp://dx.doi.org/10.1016/j.tafmec.2016.08.025pt_PT
dc.identifier.issn0167-8442
dc.identifier.urihttp://hdl.handle.net/10400.21/6909
dc.language.isoengpt_PT
dc.peerreviewedyespt_PT
dc.publisherElsevierpt_PT
dc.relation.publisherversionhttp://ac.els-cdn.com/S0167844216301203/1-s2.0-S0167844216301203-main.pdf?_tid=461b14f8-1a02-11e7-9031-00000aacb35d&acdnat=1491398452_ee19aabbe5a82a13b5395ddd0bad4c15pt_PT
dc.subjectFracturept_PT
dc.subjectFatiguept_PT
dc.subjectIn-phasept_PT
dc.subjectOut-of-phasept_PT
dc.subjectBiaxialpt_PT
dc.subjectCruciformpt_PT
dc.titleNumerical study of in-plane biaxial fatigue crack growth with different phase shift angle loadings on optimal specimen geometriespt_PT
dc.typejournal article
dspace.entity.typePublication
oaire.citation.endPage25pt_PT
oaire.citation.issuePart Apt_PT
oaire.citation.startPage16pt_PT
oaire.citation.titleTheoretical and Applied Fracture Mechanicspt_PT
oaire.citation.volume85pt_PT
person.familyNameMadeira
person.givenNameJose Firmino Aguilar
person.identifier.ciencia-id6F1E-DCF0-D6EC
person.identifier.orcid0000-0001-9523-3808
person.identifier.ridN-6918-2016
person.identifier.scopus-author-id7003405549
rcaap.rightsclosedAccesspt_PT
rcaap.typearticlept_PT
relation.isAuthorOfPublicationd495619a-a6ab-4ff5-8e70-3a1351f934dc
relation.isAuthorOfPublication.latestForDiscoveryd495619a-a6ab-4ff5-8e70-3a1351f934dc

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