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Finite element modeling and critical plane analysis of a cut-and-chip experiment for rubber

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dc.title Finite element modeling and critical plane analysis of a cut-and-chip experiment for rubber en
dc.contributor.author Robertson, Christopher G.
dc.contributor.author Suter, Jesse D.
dc.contributor.author Bauman, Mark A.
dc.contributor.author Stoček, Radek
dc.contributor.author Mars, William V.
dc.relation.ispartof Tire Science and Technology
dc.identifier.issn 0090-8657 Scopus Sources, Sherpa/RoMEO, JCR
dc.date.issued 2021
utb.relation.volume 49
utb.relation.issue 2
dc.citation.spage 128
dc.citation.epage 145
dc.type article
dc.language.iso en
dc.publisher Tire Soc Inc
dc.identifier.doi 10.2346/tire.20.190221
dc.relation.uri https://meridian.allenpress.com/tst/article-abstract/49/2/128/447982/Finite-Element-Modeling-and-Critical-Plane
dc.subject durability en
dc.subject predictive testing en
dc.subject simulation en
dc.subject rubber fracture mechanics en
dc.subject tire treads en
dc.subject abrasion en
dc.description.abstract Rubber surfaces exposed to concentrated, sliding impacts carry large normal and shearing stresses that can cause damage and the eventual removal of material from the surface. Understanding this cut-and-chip (CC) effect in rubber is key to developing improved tread compounds for tires used in off-mad or poor road conditions. To better understand the mechanics involved in the CC process, an analysis was performed of an experiment conducted on a recently introduced device, the Instrumented Chip and Cut Analyzer (ICCA), which repetitively impacts a rigid indenter against a rotating solid rubber wheel. The impact process is carefully controlled and measured on this lab instrument, so that the contact time, normal force, and shear force are all known. The numerical evaluation includes Abaqus finite element analysis (FEA) to determine the stress and strain fields during impact. The FEA results are combined with rubber fracture mechanics characteristics of the material as inputs to the Endurica CL elastomer fatigue solver, which employs critical plane analysis to determine the fatigue response of the specimen surface. The modeling inputs are experimentally determined hyperelastic stress-strain parameters, crack growth rate laws, and crack precursor sizes for carbon black-filled compounds wherein the type of elastomer is varied in order to compare natural rubber (NR). butadiene rubber (BR), and styrene-butadiene rubber (SBR). At the lower impact force, the simulation results were consistent with the relative CC resistances of NR. BR, and SBR measured using the ICCA, which followed the order BR > NR > SBR. Impact-induced temperature increases need to be considered in the fatigue analysis of the higher impact force to provide lifetime predictions that match the experimental CC resistance ranking of NR > SBR > BR. en
utb.faculty University Institute
dc.identifier.uri http://hdl.handle.net/10563/1010635
utb.identifier.obdid 43883377
utb.identifier.wok 000707038500003
utb.source J-wok
dc.date.accessioned 2021-11-01T19:57:45Z
dc.date.available 2021-11-01T19:57:45Z
utb.ou Centre of Polymer Systems
utb.contributor.internalauthor Stoček, Radek
utb.wos.affiliation [Robertson, Christopher G.; Suter, Jesse D.; Bauman, Mark A.; Mars, William, V] Endurica LLC, Findlay, OH 45840 USA; [Stocek, Radek] PRL Polymer Res Lab, Zlin, Czech Republic; [Stocek, Radek] Tomas Bata Univ Zlin, Ctr Polymer Syst, Zlin, Czech Republic
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