Small fatigue crack growth in metallic materials: A model and its application to engineering alloys

Amit Shyam, John E. Allison, Christopher J. Szczepanski, Tresa M. Pollock, J. Wayne Jones

Research output: Contribution to journalArticlepeer-review

75 Scopus citations

Abstract

Characterization of the growth behavior of small fatigue cracks is important for materials used in structurally demanding applications such as aircraft turbine discs and some automotive engine components. Here, we present a general, dislocation-based fracture mechanics approach to predict the growth rate of small fatigue cracks in metallic materials. The applicability of the model to the small fatigue crack growth behavior of four engineering alloys was examined. Small fatigue cracks were initiated and propagated, in a controlled manner, from micronotches fabricated by femtosecond pulsed laser micromachining. The results suggest that a methodology consisting of crack-tip damage accumulation and fracture provides a common framework to estimate the fatigue crack propagation lifetime of structural materials.

Original languageEnglish
Pages (from-to)6606-6616
Number of pages11
JournalActa Materialia
Volume55
Issue number19
DOIs
StatePublished - Nov 2007

Funding

Various segments of this investigation at the University of Michigan were supported by NSF, DARPA, AFOSR and Ford Motor Company. We thank Christopher J. Torbet and Yoosuf N. Picard of the University of Michigan for assistance with the experiments. A.S. thanks Edgar Lara-Curzio (ORNL) for reading an initial draft of the manuscript.

FundersFunder number
National Science Foundation
Air Force Office of Scientific Research
Defense Advanced Research Projects Agency
Ford Motor Company

    Keywords

    • Fatigue
    • Metals and alloys
    • Modeling
    • Plastic deformation
    • Small fatigue crack growth

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