Finite element analysis of free vibration of rectangular composite plates

This report presents a comprehensive investigation into the free vibration characteristics of rectangular composite plates using finite element analysis (FEA). The goal of the research is to better understand these structures' dynamic behavior, which is essential for improving their design...

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Main Author: Tay, Leroy Shi Han
Other Authors: Chai Gin Boay
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2024
Subjects:
Online Access:https://hdl.handle.net/10356/177776
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Institution: Nanyang Technological University
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spelling sg-ntu-dr.10356-1777762024-06-01T16:54:14Z Finite element analysis of free vibration of rectangular composite plates Tay, Leroy Shi Han Chai Gin Boay School of Mechanical and Aerospace Engineering MGBCHAI@ntu.edu.sg Engineering This report presents a comprehensive investigation into the free vibration characteristics of rectangular composite plates using finite element analysis (FEA). The goal of the research is to better understand these structures' dynamic behavior, which is essential for improving their design and guaranteeing structural integrity in a range of technical applications. A three-dimensional thin laminated shell finite element model is developed and implemented as part of the study technique, considering the anisotropic character of composite materials. To investigate the effects of important parameters on the natural frequencies and mode forms of the composite plates, including plate dimensions, stacking order, and material properties, parametric research is carried out. The vibrational response of rectangular composite plates is influenced by a complex interaction of geometric and material parameters, as demonstrated by the results of the finite element analysis. Furthermore, the distribution of nodal patterns and deformation modes is revealed by the modal analysis, which helps identify crucial places that may experience resonance and eventual failure. Moreover, analytical solutions, experimental data, and FEA predictions are compared to verify the precision and dependability of the created finite element model. The results of this study make a significant contribution to the field of composite plate dynamics and provide insightful advice to engineers and designers who aim to improve the longevity and performance of structures made of composite materials. In a nutshell, this study's result emphasizes the value of using finite element analysis to thoroughly examine the properties of free vibration in rectangular composite plates. The knowledge gained serves to support the continuous efforts to optimize composite structures, guaranteeing their effective use in a variety of engineering applications. Bachelor's degree 2024-05-31T05:33:01Z 2024-05-31T05:33:01Z 2024 Final Year Project (FYP) Tay, L. S. H. (2024). Finite element analysis of free vibration of rectangular composite plates. Final Year Project (FYP), Nanyang Technological University, Singapore. https://hdl.handle.net/10356/177776 https://hdl.handle.net/10356/177776 en application/pdf Nanyang Technological University
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering
spellingShingle Engineering
Tay, Leroy Shi Han
Finite element analysis of free vibration of rectangular composite plates
description This report presents a comprehensive investigation into the free vibration characteristics of rectangular composite plates using finite element analysis (FEA). The goal of the research is to better understand these structures' dynamic behavior, which is essential for improving their design and guaranteeing structural integrity in a range of technical applications. A three-dimensional thin laminated shell finite element model is developed and implemented as part of the study technique, considering the anisotropic character of composite materials. To investigate the effects of important parameters on the natural frequencies and mode forms of the composite plates, including plate dimensions, stacking order, and material properties, parametric research is carried out. The vibrational response of rectangular composite plates is influenced by a complex interaction of geometric and material parameters, as demonstrated by the results of the finite element analysis. Furthermore, the distribution of nodal patterns and deformation modes is revealed by the modal analysis, which helps identify crucial places that may experience resonance and eventual failure. Moreover, analytical solutions, experimental data, and FEA predictions are compared to verify the precision and dependability of the created finite element model. The results of this study make a significant contribution to the field of composite plate dynamics and provide insightful advice to engineers and designers who aim to improve the longevity and performance of structures made of composite materials. In a nutshell, this study's result emphasizes the value of using finite element analysis to thoroughly examine the properties of free vibration in rectangular composite plates. The knowledge gained serves to support the continuous efforts to optimize composite structures, guaranteeing their effective use in a variety of engineering applications.
author2 Chai Gin Boay
author_facet Chai Gin Boay
Tay, Leroy Shi Han
format Final Year Project
author Tay, Leroy Shi Han
author_sort Tay, Leroy Shi Han
title Finite element analysis of free vibration of rectangular composite plates
title_short Finite element analysis of free vibration of rectangular composite plates
title_full Finite element analysis of free vibration of rectangular composite plates
title_fullStr Finite element analysis of free vibration of rectangular composite plates
title_full_unstemmed Finite element analysis of free vibration of rectangular composite plates
title_sort finite element analysis of free vibration of rectangular composite plates
publisher Nanyang Technological University
publishDate 2024
url https://hdl.handle.net/10356/177776
_version_ 1814047319762403328