Abstract

The contribution of residual compressive stresses induced by shot peening to the improvement in fatigue life of Al 2024 is assessed. Shot peening results in an increase in dislocation density and in compressive residual stresses at the surface. Propagation rates of small surface cracks were measured in the electrolytically polished (reference) and shot peened conditions, and were found to be drastically reduced after shot peening. A minimum in propagation rates for shot peened specimens is found where the cracks propagate through the region of maximum residual compressive stresses. Comparison of these results with those of other materials indicates that the effect of residual compressive stresses on fatigue life in Al 2024 is far more pronounced than has been previously thought.

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