Recent advances in piezoelectric wafer active sensors for structural health monitoring applications

H Mei, MF Haider, R Joseph, A Migot, V Giurgiutiu - Sensors, 2019 - mdpi.com
In this paper, some recent piezoelectric wafer active sensors (PWAS) progress achieved in
our laboratory for active materials and smart structures (LAMSS) at the University of South …

Quantitative modeling of coupled piezo-elastodynamic behavior of piezoelectric actuators bonded to an elastic medium for structural health monitoring: A review

G Huang, F Song, X Wang - Sensors, 2010 - mdpi.com
Elastic waves, especially guided waves, generated by a piezoelectric actuator/sensor
network, have shown great potential for on-line health monitoring of advanced aerospace …

Structural health monitoring (SHM) of aerospace composites

V Giurgiutiu - Polymer composites in the aerospace industry, 2020 - Elsevier
The chapter deals with structural health monitoring (SHM) of aerospace composites. After a
brief introduction, the discussion focuses on the significant types of aerospace composite …

A stretchable and large-scale guided wave sensor network for aircraft smart skin of structural health monitoring

Y Wang, L Qiu, Y Luo, R Ding - Structural Health Monitoring, 2021 - journals.sagepub.com
Aircraft smart skin technology requires the integration of large-scale, lightweight, and
integrative sensor networks with aircraft structural skin, but it is difficult to directly …

Delamination detection and quantification on laminated composite structures with Lamb waves and wavenumber analysis

Z Tian, L Yu, C Leckey - Journal of Intelligent Material …, 2015 - journals.sagepub.com
Laminated composites are susceptible to delamination due to their weak transverse tensile
and interlaminar shear strengths as compared to their in-plane properties. Delamination …

Locating fatigue damage using temporal signal features of nonlinear Lamb waves

M Hong, Z Su, Y Lu, H Sohn, X Qing - Mechanical Systems and Signal …, 2015 - Elsevier
The temporal signal features of linear guided waves, as typified by the time-of-flight (ToF),
have been exploited intensively for identifying damage, with proven effectiveness in locating …

Optimal sensor placement for maximum area coverage (MAC) for damage localization in composite structures

M Thiene, ZS Khodaei… - Smart materials and …, 2016 - iopscience.iop.org
In this paper an optimal sensor placement algorithm for attaining the maximum area
coverage (MAC) within a sensor network is presented. The proposed novel approach takes …

Identification of disbond and high density core region in a honeycomb composite sandwich structure using ultrasonic guided waves

S Sikdar, S Banerjee - Composite Structures, 2016 - Elsevier
The aim of this study is to identify disbond and high-density (HD) core region in a
honeycomb composite sandwich structure (HCSS) using ultrasonic guided waves (GWs) …

Fourier spectral-based modal curvature analysis and its application to damage detection in beams

ZB Yang, M Radzienski, P Kudela… - Mechanical systems and …, 2017 - Elsevier
In this paper, a simple Fourier spectral-based method is proposed to calculate the modal
curvature (MC) of beams instead of the traditional central difference method. Based on the …

Impact imaging of aircraft composite structure based on a model-independent spatial-wavenumber filter

L Qiu, B Liu, S Yuan, Z Su - Ultrasonics, 2016 - Elsevier
The spatial-wavenumber filtering technique is an effective approach to distinguish the
propagating direction and wave mode of Lamb wave in spatial-wavenumber domain …