Damage localisation in a stiffened composite panel

D. Chetwynd, F. Mustapha, K. Worden, J.A. Rongong, Janice M Barton

Research output: Contribution to journalArticle (Academic Journal)

Abstract

This work was conducted as part of the Aircraft Reliability Through Intelligent Materials Application (ARTIMA) European Union project. It presents a case study of damage detection in a curved carbon-fibre reinforced panel with two omega stiffeners which was investigated using ultrasonic Lamb waves. The statistical technique of outlier analysis was used here as a way of pre-processing experimental data prior to damage classification. Multilayer perceptron neural networks were used here for both classification and regression problems of damage detection. It was then investigated whether using wavelet analysis to perform prior wavelet decompositions of experimental data could facilitate damage classification.
Original languageUndefined/Unknown
Pages (from-to)298-307
Number of pages10
JournalStrain
Volume44
Issue number4
Publication statusPublished - 1 Aug 2008

Keywords

  • damage detection, multilayer perceptron, outlier analysis, wavelet decomposition

Cite this

Chetwynd, D., Mustapha, F., Worden, K., Rongong, J. A., & Barton, J. M. (2008). Damage localisation in a stiffened composite panel. Strain, 44(4), 298-307. https://eprints.soton.ac.uk/55268/