title: Multi-frequency local wavenumber analysis and ply correlation of delamination damage.
abstract: Wavenumber domain analysis through use of scanning laser Doppler vibrometry has been shown to be effective for non-contact inspection of damage in composites. Qualitative and semi-quantitative local wavenumber analysis of realistic delamination damage and quantitative analysis of idealized damage scenarios (Teflon inserts) have been performed previously in the literature. This paper presents a new methodology based on multi-frequency local wavenumber analysis for quantitative assessment of multi-ply delamination damage in carbon fiber reinforced polymer (CFRP) composite specimens. The methodology is presented and applied to a real world damage scenario (impact damage in an aerospace CFRP composite). The methodology yields delamination size and also correlates local wavenumber results from multiple excitation frequencies to theoretical dispersion curves in order to robustly determine the delamination ply depth. Results from the wavenumber based technique are validated against a traditional nondestructive evaluation method.
authors.affiliation: Nondestructive Evaluation Sciences Branch, NASA Langley Research Center, Hampton, VA, USA.
authors.forename: Peter D
authors.initials: PD
authors.lastname: Juarez
authors.affiliation: Nondestructive Evaluation Sciences Branch, NASA Langley Research Center, Hampton, VA, USA. Electronic address: cara.ac.leckey@nasa.gov.
authors.forename: Cara A C
authors.initials: CA
authors.lastname: Leckey
keywords: Composite; Delamination; Guided waves; Laser vibrometer; Wavenumber