Fatigue crack growth micromechanisms are studied in 25Kh1M1F/15Kh13MF bimetal specimens with a side notch with asymmetry cycle R = 0. The main features are established for the geometric ratio of fatigue groove width and depth around the 25Kh1M1F/15Kh13MF bimetal interface.
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Translated from Metallurg, No. 1, pp. 63–67, January, 2014.
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Maruschak, P.O., Konovalenko, I.V., Maruschak, E.V. et al. Automated Method for Stereometric Study of Fatigue Failure Mechanisms. Metallurgist 58, 43–47 (2014). https://doi.org/10.1007/s11015-014-9866-6
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DOI: https://doi.org/10.1007/s11015-014-9866-6