Detection of cracks at rivet holes using guided waves

Guided Lamb waves can be used for a fast inspection of large areas, e.g. the detection of cracks at rivet holes in the fuselage of airplanes. When the guided wave hits a discontinuity like a hole, a typical scattered displacement field is obtained. A change of the scattered field indicates the development of a crack. In the experiments, the first anti-symmetric mode A0 of Lamb waves in plates is excited selectively by means of a piezoelectric transducer. The used frequency range is below the cut-off frequencies of higher wave modes. The scattered field around undamaged and damaged holes is measured on a grid around the hole with a heterodyne laser interferometer. Two types of damage are introduced: a notch cut with a very fine saw blade, and a fatigue grown crack. A significant change in the scattered field due to the defect is seen. Good agreement of the experimental results with theoretical calculations is obtained. The wave propagation is studied using Mindlin's theory of plates. The scattered field is calculated analytically and using finite difference methods (FDMs).