Abstract
The growth rate of a fatigue crack is modelled from a damage accumulation standpoint. The material ahead of the crack-tip is considered to be composed of assembly of uniaxial fatigue elements which accumulate damage per load cycle. Each element is subjected to increased levels of stress and strain ranges as the crack propagates. A linearly accumulated damage criterion is assumed, and failure of an element indicates a void initiation at its position. Both deterministic and stochastic analyses are included. The historical damage of the material before it reaches the crack tip vicinity is quantified and is shown to be significant for the first few elements. The predicted results agree fairly well with the experimental data.
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