Abstract

The comparison of shear stress determination methods in tubular specimens under torsion is presented in this paper. Four methods were analyzed: purely elastic solutions, purely plastic solutions, the midsection approach, and the Chaboche nonlinear kinematic hardening model. Using experimental data from self-designed and conducted fatigue experiments, an interesting insight on this problem was obtained that is not often tackled in the literature. It was shown that there are differences in determined shear stress values, and their level depends on a few factors. The midsection approach and purely plastic solution gave values of surface shear stress very close to the values obtained using the Chaboche nonlinear kinematic hardening model for high strain levels. The purely elastic solution gave proper results for the low strain ranges, close to the cyclic yield limit. Since none of the methods can be trusted in the full range of loading, an important conclusion from these analyses regards the formulated ranges of their applicability. It was also shown that the calculated values of shear stress and plastic and elastic strain energy density determined on this basis have a strong impact on fatigue life predictions. Finally, the influence of predicted values of shear stresses on the interpretation of cyclic hardening phenomena was also presented.

Highlights

  • Fatigue cracks originate on a free surface due to the stress concentration on a micro and macro scale

  • None of the considered approximate solutions can determine the exact value of surface shear stress for tubular specimens under elastic–plastic cyclic torsional loading

  • Using the midsection approach and purely plastic solution for high strain levels, it was found that values of surface shear stress were very close to the values obtained using the Chaboche nonlinear kinematic model, calibrated using the experimental data for the axial loading

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Summary

Introduction

Fatigue cracks originate on a free surface due to the stress concentration on a micro and macro scale. In the case of elements that are loaded with bending moment or torque, stresses are higher on a surface due to their gradient [2,3]. These types of loading are often studied [4,5], in an elastic–plastic strain range [6,7]. It is clear that the proper analysis of stress and strain on the surface of elements undergoing fatigue loading is an important issue. A compromise between the accuracy and simplicity of the solution is usually desired

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