Abstract

This paper presents a new methodology for detecting and quantifying delamination in composite plates based on the high-frequency local vibration under the excitation of piezoelectric wafer active sensors. Finite-element-method-based numerical simulations and experimental measurements were performed to quantify the size, shape, and depth of the delaminations. Two composite plates with purpose-built delaminations of different sizes and depths were analyzed. In the experiments, ultrasonic C-scan was applied to visualize the simulated delaminations. In this methodology, piezoelectric wafer active sensors were used for the high-frequency excitation with a linear sine wave chirp from 1 to 500 kHz and a scanning laser Doppler vibrometer was used to measure the local vibration response of the composite plates. The local defect resonance frequencies of delaminations were determined from scanning laser Doppler vibrometer measurements and the corresponding operational vibration shapes were measured and utilized to quantify the delaminations. Harmonic analysis of local finite element model at the local defect resonance frequencies demonstrated that the strong vibrations only occurred in the delamination region. It is shown that the effect of delamination depth on the detectability of the delamination was more significant than the size of the delamination. The experimental and finite element modeling results demonstrate a good capability for the assessment of delamination with different sizes and depths in composite structures.

Highlights

  • Composite materials have been extensively used in aerospace structures due to their high specific strength and stiffness, resistance to corrosion, light weight, and design flexibility [1]

  • A new methodology is presented to detect and quantify the size, shape, and depth of delamination in composite structures based on the high-frequency local vibration under

  • The C-scan image shows that the circular delamination C had a light blue color map, which means that the delamination was close to the bottom surface

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Summary

Introduction

Composite materials have been extensively used in aerospace structures due to their high specific strength and stiffness, resistance to corrosion, light weight, and design flexibility [1]. Only low-frequency (modal) excitation using PWAS transducers has been conducted in the above-mentioned literature To overcome this issue, the concept of local defect resonance, as first described by Solodov in [44], has recently gained considerable attention for the detection of delamination in composites [45,46,47,48,49,50]. A new methodology is presented to detect and quantify the size, shape, and depth of delamination in composite structures based on the high-frequency local vibration under. Measured operational vibration shapes of the composite plate at the resonance frequencies of delaminations are extracted and utilized to detect and quantify the delamination. The effects of size and depth of delamination on the measured operational vibration shapes are investigated. In the thepresent present study, six cases of delaminations of different and depths were investigated

Cross-Ply Composite Plate
Schematic of amm
Unidirectional Composite
NDT Detection on the Cross-Ply Composite Plate
Schematic of non-destructive
NDT Detection on the Unidirectional Composite Plate
SLDV Measurement on the Cross-Ply Composite Plate
SLDV Measurement on the Unidirectional Composite Plate
12. The each scanning plate was similar to the first in Section as
Finite
Finite Element Model for the Cross-Ply Composite Plate
Vibration-Based Delamination Detection of Composite Plates
18. Comparison of measured operational vibration shapes cross-ply
Delamination
Conclusions
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