Numerical Investigation on Guided Waves Dispersion and Scattering Phenomena in Stiffened Panels

The aim of this work is to propose a numerical methodology based on the finite element (FE) method to investigate the dispersive behavior of guided waves transmitted, converted, and reflected by reinforced aluminum and composite structures, highlighting their differences. The dispersion curves of such modes can help designers in improving the damage detection sensitivity of Lamb wave based structural health monitoring (SHM) systems. A preliminary phase has been carried out to assess the reliability of the modelling technique. The accuracy of the results has been demonstrated for aluminum and composite flat panels by comparing them against experimental tests and semi-analytical data, respectively. Since the good agreement, the FE method has been used to analyze the phenomena of dispersion, scattering, and mode conversion in aluminum and composite panels characterized by a structural discontinuity, as a stiffener. The research activity allowed emphasizing modes conversion at the stiffener, offering new observations with respect to state of the art. Converted modes propagate with a slightly slower speed than the incident ones. Reflected waves, instead, have been found to travel with the same velocity of the incident ones. Moreover, waves reflected in the composite stiffened plate appeared different from those that occurred in the aluminum one for the aspects herein discussed.

Automated summary

This study proposed a numerical methodology based on the finite element method to investigate the dispersive behavior of guided waves in reinforced aluminum and composite structures, which can improve the damage detection sensitivity of Lamb wave based structural health monitoring systems. The accuracy of the method was demonstrated through comparison with experimental tests and semi-analytical data. The research highlighted the mode conversion at stiffeners and differences in reflected waves between aluminum and composite panels.