| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 856680 | Procedia Engineering | 2015 | 9 Pages |
Abstract
Fatigue crack growth behavior of a series of aluminum alloy under single overload tests, repeated overload tests and a variable amplitude loading spectrum are analyzed. It is shown that the material behavior is governed by micro-mechanisms. For crack initiation at a notch, a short crack model presented here gives acceptable results.
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