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 language | English |
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Pages (from-to) | 6606-6616 |
Number of pages | 11 |
Journal | Acta Materialia |
Volume | 55 |
Issue number | 19 |
DOIs | |
State | Published - 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.
Funders | Funder number |
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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