A NOTE ON MODELING SHORT FATIGUE-CRACK BEHAVIOR

Based upon experimental short fatigue crack growth data and adopting t he Brown-Hobson model, new crack growth equations have been derived in an attempt to describe more precisely short fatigue crack growth beha viour that separates the physically small crack regime from the long c rack regime. An empirical model for physically small crack growth was developed by employing elastic-plastic fracture mechanics parameters. By considering the proposed approach to short fatigue crack modelling, a new second 'microstructural' threshold condition has been establish ed using only short fatigue crack growth data. In the case of fatigue in an aggressive environment it is suggested that three transition (th reshold) conditions can be identified representing: (i) a stress-assis ted pitting/pit-to-crack transition; (ii) a microstructurally short sh ear crack/physically small tensile crack transition; and (iii) a physi cally small crack/long crack transition. A comparison of this approach with that of existing models has been made, and predictions of total fatigue lifetime using the model have been presented. A reasonable agr eement has been observed between predicted and experimental crack grow th rates.