Technical Papers
Sep 26, 2024

Virtual Frequency Fusion Technique: Detecting Multiple Damages via Broadband Lamb Wave Field Using Scanning Laser Vibrometry

Publication: Journal of Aerospace Engineering
Volume 38, Issue 1

Abstract

This article presents an efficient frequency fusion method by virtual acquisition of multifrequency guided wave velocity data for robust and accurate localization of multiple damages in plate-like structures. Lamb waves are actuated by applying voltage excitation to piezoelectric patch transducers affixed on the plate, and the velocity response is measured using the noncontact scanning laser Doppler vibrometer (SLDV). The results show that the usual root mean square (RMS) and weighted RMS maps of the velocity field measured using a single narrowband pulse excitation of a given central frequency may not accurately localize multiple damages. To overcome this challenge, we propose a fusion method in the form of the product of normalized reciprocal root mean square (rRMS) maps at multiple narrowband excitation frequencies for combining the measurement data from the different excitation frequencies. However, SLDV measurements at multiple narrowband frequencies would be tedious, time-consuming, and expensive. This difficulty is eliminated by virtually computing the velocity fields at various narrowband frequencies from a single physical measurement using broadband excitation. The efficacy of the proposed method is verified through the experimental investigation on an aluminum plate with multiple damages of different shapes and orientations for two different damage scenarios. The method could identify all damages accurately and clearly through sharp peaks in the rRMS amplitude at the damage locations without any accompanying ripples near them. On the other hand, the RMS and weighted RMS maps do not perform as well even after applying fusion of multiple frequencies.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

Acknowledgments

S. Kapuria acknowledges the financial support for this work provided by the Science and Engineering Research Board, Department of Science and Technology, Government of India through J. C. Bose National Fellowship (Grant No. JBR/2023/000025) and Core Research Grant (CRG/2021/001237). This paper has been assigned the registration number CSIR-SERC-1034/2023. M. Kannusamy and S. Sasmal acknowledge the generous grant from CSIR, New Delhi, for this research.

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Information & Authors

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 38Issue 1January 2025

History

Received: Feb 28, 2024
Accepted: Jul 18, 2024
Published online: Sep 26, 2024
Published in print: Jan 1, 2025
Discussion open until: Feb 26, 2025

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Authors

Affiliations

M. Kannusamy [email protected]
Senior Scientist, Special and Multifunctional Structures Laboratory, Council of Scientific and Industrial Research-Structural Engineering Research Centre, Taramani, Chennai 600113, Tamil Nadu, India; Academy of Scientific and Innovative Research, Ghaziabad, Uttar Pradesh 201002, India. Email: [email protected]
Chief Scientist and Head, Special and Multifunctional Structures Laboratory, Council of Scientific and Industrial Research-Structural Engineering Research Centre, Taramani, Chennai 600113, Tamil Nadu, India; Academy of Scientific and Innovative Research, Ghaziabad, Uttar Pradesh 201002, India. ORCID: https://orcid.org/0000-0002-6780-3567. Email: [email protected]
Professor and Head, Dept. of Applied Mechanics, Indian Institute of Technology Delhi, Hauz Khas, New Delhi 110016, India (corresponding author). ORCID: https://orcid.org/0000-0003-1172-1279. Email: [email protected]

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