Abstract
As a result of the study performed, it has been found that for assessing the influence of surface hardening on the fatigue limit for the parts of different diameters made of steel 20, it is advisable to use a criterion for mean integral residual stresses.
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Pavlov, V.F., Kirpichev V.A., and Vakulyuk, V.S., Prognozirovanie soprotivleniya ustalosti poverkhnostno uprochennykh detalei po ostatochnym napryazheniyam (Fatigue Resistance Prediction for Surface Hardened Parts by Residual Stresses), Samara: Izd. SNTs RAN, 2012.
Pavlov, V.F., On the Relation between Residual Stresses and Fatigue Limit in Bending under Stress Concentration Conditions, Izv.Vuz. Mashinostroenie, 1986, no. 8, pp. 29–32.
Ivanov, S.I., Shatunov, M.P., and Pavlov, V.F., The Influence of Residual Stresses on Fatique Life of Notched Specimens, in Voprosy prochnosti elementov aviatsionnykh konstruktsii (Problems of Aircraft Construction Elements Strength), Kuibyshev: KuAI, 1974, issue 1, pp. 88–95.
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Original Russian Text ©V.F. Pavlov, V.A. Kirpichev, V.S. Vakulyuk, V.P. Sazanov, 2014, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2013, No. 3, pp. 79–80
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Pavlov, V.F., Kirpichev, V.A., Vakulyuk, V.S. et al. Surface hardening influence on the fatigue limit for cylindrical parts of different diameter. Russ. Aeronaut. 57, 324–326 (2014). https://doi.org/10.3103/S1068799814030180
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DOI: https://doi.org/10.3103/S1068799814030180