1985
DOI: 10.1111/j.1460-2695.1985.tb00428.x
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The Low Cycle Impact Fatigue Properties of Pearlitic Plain Carbon Steels

Abstract: The results of Stanton and Bairstow (1908) have been reanalyzed to yield information on the composition dependence of the low cycle impact fatigue properties of pearlitic plain carbon steels. It has been found that the energy absorbed per impact, E,, and the number of impacts to failure, N,, are related by the equation:In this equation q is determined by the carbon, manganese and silicon contents of the steel; E,, is the impact endurance limit; and C and D are constants. The curve represented by this equation … Show more

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Cited by 9 publications
(4 citation statements)
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“…E t -N f ) to the S-N relationship that is observed in the standard fatigue tests of metallic materials. Based on the results reported in this work Johnson and Johnson [2] showed that the following equation is valid as a description for the energy corresponding to cyclic impact loading.…”
Section: Introductionmentioning
confidence: 84%
“…E t -N f ) to the S-N relationship that is observed in the standard fatigue tests of metallic materials. Based on the results reported in this work Johnson and Johnson [2] showed that the following equation is valid as a description for the energy corresponding to cyclic impact loading.…”
Section: Introductionmentioning
confidence: 84%
“…where T ref is a reference temperature, T melt is the melting temperature, m is a softening exponent, a 2 and a 3 are model constants. The expression in the second set of brackets (equation 4) is proposed by Johnson and Cook [6] to describe the dependence of the von Mises flow stress on temperature.…”
Section: Semi-empirical Plasticity Modelmentioning
confidence: 99%
“…The resulting curves were found to be similar in shape to the conventional curves obtained in fatigue experiments. Johnson et al [9,10] showed that high cycle impact fatigue was governed by the following equation: where is the energy absorbed per impact, is the impact fatigue limit, is the number of impacts to failure, and and are known as the impact fatigue parameter and impact fatigue exponent, respectively.…”
Section: Introductionmentioning
confidence: 99%