Experiment and modeling of uniaxial tension fatigue performances for filled natural rubbers

Shangguan, Wen‐Bin; Wang, Xiaoli; Deng, Jianxiang; Rakheja, Subhash; Pan, Xiaoyong; Yu, Bingxin

doi:10.1016/j.matdes.2014.01.035

Cited by 44 publications

(55 citation statements)

References 16 publications

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“…The fatigue life [29,30] of rubber composites under the condition of maximum strain 150% were obtained through fatigue testing machine (FT3000-2, Beijing Ruida Yuchen Co., Ltd, Beijing, China), according to ISO 6943:2007.…”

Section: Methodsmentioning

confidence: 99%

Characterization and Quantitative Analysis of Crack Precursor Size for Rubber Composites

Guo

Wen

et al. 2019

Materials

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In the field of engineering, the annual economic loss caused by material fatigue failure reaches 4% of the total economic output. The deep understanding of rubber fatigue failure can help develop and prepare rubber composites with high durability. The crack precursor sizes within the rubber composites are vital for the material mechanical and fatigue properties. In this study, we adopted three different characterization methods to analyze crack precursor sizes and their distribution. First, based on the theoretical formula of fracture mechanics, the size of the crack precursor was deduced from 180 μm to 500 μm by the uniaxial tensile experiment combined with tear test (nicked angle tear, planar tear and trouser tear). Second, by combining the uniaxial fatigue test of dumbbell specimen with the fatigue crack growth rate test, the average size of the crack precursor was calculated as 3.3 μm based on the Thomas fatigue crack growth model. Third, the average size of the crack precursor was 3.6 μm obtained by scanning electron microscope. Through theoretical calculations and experimental tests, the size and distribution of the crack precursors of rubber composites were systematically presented. This work can provide theoretical guidance for the improvement of fatigue performance of rubber composites.

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Section: Methodsmentioning

confidence: 99%

Characterization and Quantitative Analysis of Crack Precursor Size for Rubber Composites

Guo

Wen

et al. 2019

Materials

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“…The method based on continuum mechanics is relatively simpler since the stresses or the strains can be easily determined from a finite element (FE) model of the rubber. Shangguan et al 3 measured the fatigue lives of various dumbbell rubber specimens and employed different measures of the strain (the peak principal strain and the peak octahedral shear strain) and the peak strain energy density as the damage parameters to model the fatigue life of rubbers. The peak strain or the peak strain energy density measures, however, are considered valid for predicting the fatigue life of rubbers only at room temperature.…”

Section: Damage Parametersmentioning

confidence: 99%

Measurement and modelling of the fatigue life of rubber mounts for an automotive powertrain at high temperatures

Duan

Shangguan

et al. 2015

Proceedings of the Institution of Mechanical Engineers, Part D:

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A fatigue experiment is carried out on filled natural rubber specimens with two different Shore hardnesses (45 and 50) and three different temperatures (23°C, 60°C and 90°C) under uniaxial tension loads. The measured fatigue life data obtained under different displacement loads are used to formulate fatigue life prediction models corresponding to different operating temperatures for the two hardnesses using the peak engineering strain as the damage parameter. The influences of the temperature, the stress softening at high temperatures and the hardness on the fatigue life of rubbers are measured and discussed. The proposed models are used to predict the fatigue life of a rubber mount for a powertrain mounting system. The validity of the prediction model is demonstrated by comparisons with the measured fatigue life data of the rubber mount at 90°C. A method for determining the damage parameters required for predicting the fatigue life is presented on the basis of the finite element model of the rubber mount. The Mooney-Rivlin constitutive constants of the hyperelastic rubber material are identified on the basis of the measured data on the specimens. Comparisons of the measured and the estimated fatigue lives of the rubber mount at 90°C revealed reasonably good agreement. The ratio of the predicted fatigue life to the measured fatigue life was within a factor of 2 under the range of loading conditions considered.

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“…Substituting Equations (12) and (13) into Equation 3, the CED increment, function of the crack angle θ, principal stretch ratio λ 1 and biaxial parameter B, is expressed as follows:…”

Section: Ced Calculation Under Finite Strainmentioning

confidence: 99%

“…In fact, Shangguan et al [13] established a generalized relationship between the fatigue life of rubber and the maximum principal Green Lagrange strain. It was found that this criterion was the most appropriate to predict fatigue life of rubbers, under uniaxial loading, independently of the specimen geometry.…”

Section: Introductionmentioning

confidence: 99%

Cracking energy density for rubber materials: Computation and implementation in multiaxial fatigue design

Belkhiria

Hamdi

Fathallah

2020

Polymer Engineering & Sci

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This article proposes a heuristic model to predict the fatigue life of rubber parts. The developed model is mainly based on the Cracking Energy Density (CED), originally developed by Mars, for the study of rubber parts fatigue. The main contribution consists in the integration of the theoretical framework of the critical plane analysis proposed by Mars with Saintier's experimental research carried out in tension and torsion modes. The CED parameter, derived from the Strain Energy Density (SED), can predict the occurrence of the first crack and its possible orientation depending on the type of loading path. In this context, an analytical analysis of this parameter is carried out for typical loading cases. Furthermore, the variation of CED by SED ratio (WC/W), as a function of the probable crack angle θ and the principal stretch λ1 is investigated. A finite element (FE) model is, then, developed to measure the performance and efficiency for some basic criteria used to investigate rubber fatigue life in literature. The pertinence of such criteria is evaluated in terms of a determination coefficient. The CED parameter can be considered as the most effective criterion for describing the multiaxial fatigue life of rubbers.

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Experiment and modeling of uniaxial tension fatigue performances for filled natural rubbers

Cited by 44 publications

References 16 publications

Characterization and Quantitative Analysis of Crack Precursor Size for Rubber Composites

Characterization and Quantitative Analysis of Crack Precursor Size for Rubber Composites

Measurement and modelling of the fatigue life of rubber mounts for an automotive powertrain at high temperatures

Cracking energy density for rubber materials: Computation and implementation in multiaxial fatigue design

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