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This paper is the first to explain how to account for the variability seen in delamination growth and how to determine the growth curve that is required by MIL-STD-1530 to assess tge effect of delamination damage in operational aircraft.
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This page is a summary of: Delamination Growth in Polymer-Matrix Fibre Composites and the Use of Fracture-Mechanics Data for Material Characterization and Life Prediction, January 2018, Elsevier,
DOI: 10.1016/b978-0-08-100540-8.00013-3.
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