2021
DOI: 10.1111/ffe.13458
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A modification of Matake criterion for considering the effect of mean shear stress under high cycle fatigue loading

Abstract: In the present paper, a brief review for some existing critical plane-based life prediction models is presented, and limitations of these models in reflecting the influence of mean stress on fatigue life are discussed. It is found that the effect of mean normal stress on fatigue damage has been well taken into account for most of the critical plane-based fatigue life prediction models, while mean shear stress effect is not well considered in these models. Therefore, a new critical plane-based multiaxial high c… Show more

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Cited by 13 publications
(14 citation statements)
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“…The statistical analysis is carried out through the probability density function (PDF), as shown in Figure 5, and the normal distribution function is selected 57,58 : f()xgoodbreak=12πσPe()xgoodbreak−μP22σP2, where μP and σP are the mean value and standard deviation of the distribution for the prediction errors Perror, respectively.…”
Section: Model Validation and Discussionmentioning
confidence: 99%
See 1 more Smart Citation
“…The statistical analysis is carried out through the probability density function (PDF), as shown in Figure 5, and the normal distribution function is selected 57,58 : f()xgoodbreak=12πσPe()xgoodbreak−μP22σP2, where μP and σP are the mean value and standard deviation of the distribution for the prediction errors Perror, respectively.…”
Section: Model Validation and Discussionmentioning
confidence: 99%
“…Δσ where N fp and N ft are the estimated and experimental life, respectively. The statistical analysis is carried out through the probability density function (PDF), as shown in Figure 5, and the normal distribution function is selected 57,58 :…”
Section: Proposed Life Prediction Modelmentioning
confidence: 99%
“…It is generally known that there exist different types of criteria and that each considers a different damage parameter that acts on the critical plane. For some stress‐based multiaxial fatigue criteria, the maximum stress amplitude and direction on the critical plane are usually used to estimate the fatigue life and crack initiation angle 179,180 . Cruces et al 181,182 investigated the multiaxial fatigue of AMed 18Ni300 using several methods:…”
Section: Non‐ml‐based Methods For Fatigue Life Prediction Of Am Metalsmentioning
confidence: 99%
“…For some stressbased multiaxial fatigue criteria, the maximum stress amplitude and direction on the critical plane are usually used to estimate the fatigue life and crack initiation angle. 179,180 Cruces et al 181,182 investigated the multiaxial fatigue of AMed 18Ni300 using several methods: Strain energy-based models Liu and Wang 183 defined the maximum normal strain energy and maximum shear strain energy at the critical plane to describe the fatigue damage dominated by mode I failure mechanism and mode II failure mechanism, respectively. Cruces et al 181 modified their forms to consider the effect of mean stress, as follows:…”
Section: Critical Plane Modelsmentioning
confidence: 99%
“…The statistical analysis is conducted through the probability density functions. As shown in Figure 5, the prediction results and the comparisons for the three models are also presented in the format of probability density functions, and the normal distribution function is selected [53][54][55] :…”
Section: Validation Of the Proposed Modelmentioning
confidence: 99%