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This document discusses fracture mechanisms that can influence fatigue crack propagation rates in aluminum alloys. It notes that analytical fatigue theories typically predict a slope of 2 for the relationship between crack growth rate and stress intensity range, but experimental results often find steeper slopes. This can be explained by additional "static" fracture modes occurring during fatigue cracking, such as cleavage cracking of brittle inclusions and void coalescence. The influence of microstructural
- Author
- Nils Verkleij
- Language
- EN