Investigation of compression after impact failure in carbon fiber reinforced polymers using acoustic emission

Journal Article (2023)
Author(s)

D. Biagini (TU Delft - Structural Integrity & Composites)

John- Alan Pascoe (TU Delft - Structural Integrity & Composites)

René C. Alderliesten (TU Delft - Structural Integrity & Composites)

Research Group
Structural Integrity & Composites
Copyright
© 2023 D. Biagini, J.A. Pascoe, R.C. Alderliesten
DOI related publication
https://doi.org/10.1177/00219983231163853
More Info
expand_more
Publication Year
2023
Language
English
Copyright
© 2023 D. Biagini, J.A. Pascoe, R.C. Alderliesten
Related content
Research Group
Structural Integrity & Composites
Issue number
10
Volume number
57
Pages (from-to)
1819-1832
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

Although several studies have been performed, the compression after impact (CAI) failure of CFRP is still not entirely understood. It is still unclear what sequence of events determines the onset of failure in CAI tests and how the different damage modes are involved in this process. To experimentally investigate this matter, the present work relies on acoustic emission (AE) monitoring and advanced acoustic signal analysis. A series of preliminary tests was conducted to correlate damage modes with recorded acoustic waveforms. Four types of waveforms were separated and associated to different damage modes. Following the preliminary tests, AE was monitored in actual CAI tests. A damage accumulation study was conducted combining three indicators, namely wavelet packet components, sentry function and energy b-value. The results evidence different phases in the damage accumulation process that were not shown in previous literature. In all specimens, the onset of the unstable damage accumulation appeared to be triggered by an intermediate frequency acoustic event associated to a combination of matrix cracking and fiber-matrix debonding, occurring at 80% of failure displacement.