620.179.1
and T. P MaslakWe present the results of our study aimed at development of a computerized optical method of evaluation of the accumulated fatigue damage. We show a possibility of predicting the residual resource of aircraft components made from clad aluminum alloys by the deformation relief of their surface near stress concentrators. For the quantitative estimation of deformation relief we use the parameters which characterize its saturation and fractal dimension.
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