Investigation of ultrasonic guided wave inspection on a wing spar structure
In recent years, ultrasonic guided waves have proven to be a reliable and fruitful method for examining large structures. The capability of inspecting areas that are unreachable or inaccessible is what gains our interest. This thesis investigates the guided wave propagation in an isotropic spar s...
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sg-ntu-dr.10356-1476342023-03-11T17:42:14Z Investigation of ultrasonic guided wave inspection on a wing spar structure Nazeer, Nakash Fan Zheng, David School of Mechanical and Aerospace Engineering ZFAN@ntu.edu.sg Engineering::Mechanical engineering In recent years, ultrasonic guided waves have proven to be a reliable and fruitful method for examining large structures. The capability of inspecting areas that are unreachable or inaccessible is what gains our interest. This thesis investigates the guided wave propagation in an isotropic spar structure. The focus is on the 0th order shear horizontal wave mode (SH0) below the cut-of frequency of SH1 mode which is 1.6 MHz-mm. A fundamental study is carried out using a 2D system examining the propagation in the straight plate part and also in the circumferential bend region. A wave mode is chosen appropriately to carry out the wave propagation characteristics. The curvature effects are examined by comparing the group velocity, displacement, stress and strain distributions between a flat and curved plate for various curvature ratios. The frequency dependence of the distributions are also looked upon. These parameters are seen to be varying across the thickness of the bend and are also frequency sensitive. Reflections arising purely from the bends are also analysed. 2D guided wave scattering from transverse defects and delamination present along the bend region are also investigated. The study is carried out in a 2D and 3D domain. The effect of frequency on the scattering is also studied. This provides a graphical tool to understand how different defect placements and sizes interact with the waves. The distribution of energy across the thickness of the bend also helps in understanding which frequency range is more sensitive to defects present towards the inner, outer or mid region of the bend. Results of Finite Element (FE) modelling were validated by experiments. Master of Science (Aerospace Engineering) 2021-04-08T02:02:23Z 2021-04-08T02:02:23Z 2016 Thesis-Master by Coursework Nazeer, N. (2016). Investigation of ultrasonic guided wave inspection on a wing spar structure. Master's thesis, Nanyang Technological University, Singapore. https://hdl.handle.net/10356/147634 https://hdl.handle.net/10356/147634 en application/pdf Nanyang Technological University |
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Engineering::Mechanical engineering Nazeer, Nakash Investigation of ultrasonic guided wave inspection on a wing spar structure |
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In recent years, ultrasonic guided waves have proven to be a reliable and fruitful
method for examining large structures. The capability of inspecting areas that are
unreachable or inaccessible is what gains our interest. This thesis investigates the
guided wave propagation in an isotropic spar structure. The focus is on the 0th order
shear horizontal wave mode (SH0) below the cut-of frequency of SH1 mode which is
1.6 MHz-mm. A fundamental study is carried out using a 2D system examining the
propagation in the straight plate part and also in the circumferential bend region. A
wave mode is chosen appropriately to carry out the wave propagation characteristics.
The curvature effects are examined by comparing the group velocity, displacement,
stress and strain distributions between a flat and curved plate for various curvature
ratios. The frequency dependence of the distributions are also looked upon. These
parameters are seen to be varying across the thickness of the bend and are also frequency
sensitive. Reflections arising purely from the bends are also analysed. 2D
guided wave scattering from transverse defects and delamination present along the
bend region are also investigated. The study is carried out in a 2D and 3D domain.
The effect of frequency on the scattering is also studied. This provides a graphical
tool to understand how different defect placements and sizes interact with the waves.
The distribution of energy across the thickness of the bend also helps in understanding
which frequency range is more sensitive to defects present towards the inner, outer or
mid region of the bend. Results of Finite Element (FE) modelling were validated by
experiments. |
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Fan Zheng, David |
author_facet |
Fan Zheng, David Nazeer, Nakash |
format |
Thesis-Master by Coursework |
author |
Nazeer, Nakash |
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Nazeer, Nakash |
title |
Investigation of ultrasonic guided wave inspection on a wing spar structure |
title_short |
Investigation of ultrasonic guided wave inspection on a wing spar structure |
title_full |
Investigation of ultrasonic guided wave inspection on a wing spar structure |
title_fullStr |
Investigation of ultrasonic guided wave inspection on a wing spar structure |
title_full_unstemmed |
Investigation of ultrasonic guided wave inspection on a wing spar structure |
title_sort |
investigation of ultrasonic guided wave inspection on a wing spar structure |
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Nanyang Technological University |
publishDate |
2021 |
url |
https://hdl.handle.net/10356/147634 |
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1761781178628571136 |