
Material property variability in carbon fiber-reinforced polymer (CFRP) composites can alter Lamb wave propagation and reduce the accuracy of quantitative delamination imaging. This study investigates the effect of material uncertainty on A0 Lamb wave time-of-flight (TOF) measurements and combines TOF-based filtered back-projection (FBP) imaging with DSMF-Canny edge extraction for quantitative delamination characterization. Numerical results show that, with an 8% deviation in elastic properties, the elliptical delamination remains well localized, with an area estimation error of 17.11% and a maximum deviation of 2 mm in the estimated damage center. These findings provide a basis for quantitative delamination assessment of CFRP structures under material uncertainty and their structural health monitoring in aerospace applications.
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