Simulation of lamb wave in composite for structural health monitoring

With the technological advancement in materials engineering, composite material has become increasingly popular for use in many industries. This leads to a need for a Structural Health Monitoring (SHM) system for composite materials. Among various SHM methods, the guided wave emerges to be a promisi...

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Main Author: Ge, Yao.
Other Authors: Guo Ningqun
Format: Final Year Project
Language:English
Published: 2009
Subjects:
Online Access:http://hdl.handle.net/10356/16877
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-168772023-03-04T18:27:09Z Simulation of lamb wave in composite for structural health monitoring Ge, Yao. Guo Ningqun School of Mechanical and Aerospace Engineering DRNTU::Engineering::Mechanical engineering::Mechanics and dynamics With the technological advancement in materials engineering, composite material has become increasingly popular for use in many industries. This leads to a need for a Structural Health Monitoring (SHM) system for composite materials. Among various SHM methods, the guided wave emerges to be a promising technology with its advantages of speed in inspection and being active in monitoring. This report presents studies on guided wave propagation using numerical simulation carried out by finite element software PZFlex. Several 2-dimensional (2D) simulations have been carried out on S¬0 and A0 Lamb wave propagation in Carbon Fiber Reinforced Plastics (CFRP), as well as piezoelectric crystal actuated Lamb wave. Good agreement has been found by comparing with theoretical and experimental results. 3-dimensional (3D) CFRP plates are modeled to study the amplitude attenuation of Lamb waves. The effect of different ply orientations: unidirectional, cross-ply and angle-ply, and different excitation areas are investigated. The rate of attenuation with units of dB/mm is obtained for each type of CFRP plate. The attenuation rate is subsequently applied to several practical structures and it is found that it is feasible to use inspect large-scale structure such as wind turbine blade and aircraft wing. Mode conversion method to locate defect is investigated with algebraic formulation, and verified by 2D and 3D simulations. The method is promising in determining the vertical notch location with the correct input of wave velocity. Further investigation is required in order to apply the method to large-scale structures with different geometry. Bachelor of Engineering (Aerospace Engineering) 2009-05-28T08:31:14Z 2009-05-28T08:31:14Z 2009 2009 Final Year Project (FYP) http://hdl.handle.net/10356/16877 en Nanyang Technological University 103 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Mechanical engineering::Mechanics and dynamics
spellingShingle DRNTU::Engineering::Mechanical engineering::Mechanics and dynamics
Ge, Yao.
Simulation of lamb wave in composite for structural health monitoring
description With the technological advancement in materials engineering, composite material has become increasingly popular for use in many industries. This leads to a need for a Structural Health Monitoring (SHM) system for composite materials. Among various SHM methods, the guided wave emerges to be a promising technology with its advantages of speed in inspection and being active in monitoring. This report presents studies on guided wave propagation using numerical simulation carried out by finite element software PZFlex. Several 2-dimensional (2D) simulations have been carried out on S¬0 and A0 Lamb wave propagation in Carbon Fiber Reinforced Plastics (CFRP), as well as piezoelectric crystal actuated Lamb wave. Good agreement has been found by comparing with theoretical and experimental results. 3-dimensional (3D) CFRP plates are modeled to study the amplitude attenuation of Lamb waves. The effect of different ply orientations: unidirectional, cross-ply and angle-ply, and different excitation areas are investigated. The rate of attenuation with units of dB/mm is obtained for each type of CFRP plate. The attenuation rate is subsequently applied to several practical structures and it is found that it is feasible to use inspect large-scale structure such as wind turbine blade and aircraft wing. Mode conversion method to locate defect is investigated with algebraic formulation, and verified by 2D and 3D simulations. The method is promising in determining the vertical notch location with the correct input of wave velocity. Further investigation is required in order to apply the method to large-scale structures with different geometry.
author2 Guo Ningqun
author_facet Guo Ningqun
Ge, Yao.
format Final Year Project
author Ge, Yao.
author_sort Ge, Yao.
title Simulation of lamb wave in composite for structural health monitoring
title_short Simulation of lamb wave in composite for structural health monitoring
title_full Simulation of lamb wave in composite for structural health monitoring
title_fullStr Simulation of lamb wave in composite for structural health monitoring
title_full_unstemmed Simulation of lamb wave in composite for structural health monitoring
title_sort simulation of lamb wave in composite for structural health monitoring
publishDate 2009
url http://hdl.handle.net/10356/16877
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