Imperial College London
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M H Ferri Aliabadi

Faculty of Engineering, Department of Aeronautics

Chair in Aerostructures
 
 
 
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Contact

 

+44 (0)20 7594 5077m.h.aliabadi

 
 
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Assistant

 

Miss Lisa Kelly +44 (0)20 7594 5056

 
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Location

 

CAGB323City and Guilds BuildingSouth Kensington Campus

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Summary

 

Publications

Citation

BibTex format

@inproceedings{Li:2018:www.scientific.net/KEM.774.625,
author = {Li, J and Khodaei, ZS and Aliabadi, MH},
doi = {www.scientific.net/KEM.774.625},
pages = {625--631},
title = {A boundary element model for structural health monitoring based on the S0 lamb wave mode},
url = {http://dx.doi.org/10.4028/www.scientific.net/KEM.774.625},
year = {2018}
}
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RIS format (EndNote, RefMan)

TY  - CPAPER
AB  - The aim of this paper was to carry out numerical simulations of structural health monitoring applications for plate structures using the boundary element method (BEM). The fundamental symmetric Lamb mode (S0) is chosen for the SHM applications. The propagation, reflection and diffraction of the S0 mode Lamb wave are modelled using a boundary element formulation based on the plane stress theory. Piezoelectric (PZT) actuators are mounted on plate surfaces to excite the S0 mode wave. A semi-analytical method is adopted to couple the PZT actuators and the host plate. Numerical results show that BEM is a very efficient simulation method for the structural health monitoring of plates.
AU  - Li,J
AU  - Khodaei,ZS
AU  - Aliabadi,MH
DO  - www.scientific.net/KEM.774.625
EP  - 631
PY  - 2018///
SN  - 1013-9826
SP  - 625
TI  - A boundary element model for structural health monitoring based on the S0 lamb wave mode
UR  - http://dx.doi.org/10.4028/www.scientific.net/KEM.774.625
ER  -
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