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NASA NTRS · 20150001232

Vibro-Acoustic Modulation Based Damage Identification in a Composite Skin-Stiffener Structure

Abstract

The vibro-acoustic modulation method is applied to a composite skin-stiffener structure to investigate the possibilities to utilize this method for damage identification in terms of detection, localisation and damage quantification. The research comprises a theoretical part and an experimental part. An impact load is applied to the skin-stiffener structure, resulting in a delamination underneath the stiffener. The structure is interrogated with a low frequency pump excitation and a high frequency carrier excitation. The analysis of the response in a frequency band around the carrier frequency is employed to assess the damage identification capabilities and to gain a better understanding of the modulations occurring and the underlying physical phenomena. Though vibro-acoustic is shown to be a sensitive method for damage identification, the complexity of the damage, combined with a high modal density, complicate the understanding of the relation between the physical phenomena and the modulations occurring. more research is recommended to reveal the physics behind the observations.

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BibTeXRIS

Ooijevaar, T. H., Loendersloot, R., Rogge, M. D., Akkerman, R., Tinga, T.. 2014-07-08. Vibro-Acoustic Modulation Based Damage Identification in a Composite Skin-Stiffener Structure. https://ntrs.nasa.gov/citations/20150001232

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