title: Non-contact ultrasonic technique for Lamb wave characterization in composite plates.
abstract: A fully non-contact single-sided air-coupled and laser ultrasonic non-destructive system based on the generation and detection of Lamb waves is implemented for the characterization of A0 Lamb wave mode dispersion in a composite plate. An air-coupled transducer (ACT) radiates acoustic pressure on the surface of the composite and generates Lamb waves within the structure. The out-of-plane velocity of the propagating wave is measured using a laser Doppler vibrometer (LDV). In this study, the non-contact automated system focuses on measuring A0 mode frequency-wavenumber, phase velocity dispersion curves using Snell's law and group velocity dispersion curves using Morlet wavelet transform (MWT) based on time-of-flight along different wave propagation directions. It is theoretically demonstrated that Snell's law represents a direct link between the phase velocity of the generated Lamb wave mode and the coincidence angle of the ACT. Using Snell's law and MWT, the former three dispersion curves of the A0 mode are easily and promptly generated from a set of measurements obtained from a rapid ACT angle scan experiment. In addition, the phase velocity and group velocity polar characteristic wave curves are also computed to analyze experimentally the angular dependency of Lamb wave propagation. In comparison with the results from the theory, it is confirmed that using the ACT/LDV system and implementing simple Snell's law method is highly sensitive and effective in characterizing the dispersion curves of Lamb waves in composite structures as well as its angular dependency.
authors.affiliation: Department of Mechanical and Aerospace Engineering, North Carolina State University, Campus Box 7910, Raleigh, NC 27695, USA; Integrated Structural Health Management Laboratory, National Institute of Aerospace, 100 Exploration Way, Hampton, VA 23666, USA.
authors.forename: M S
authors.initials: MS
authors.lastname: Harb
authors.affiliation: Department of Mechanical and Aerospace Engineering, North Carolina State University, Campus Box 7910, Raleigh, NC 27695, USA; Integrated Structural Health Management Laboratory, National Institute of Aerospace, 100 Exploration Way, Hampton, VA 23666, USA. Electronic address: yuan@ncsu.edu.
authors.forename: F G
authors.initials: FG
authors.lastname: Yuan
keywords: Air-coupled ultrasound; Composites; Dispersion curves; Lamb waves; Snell’s law