Finite element analysis of the buckling of rectangular composite plates in compression

This project is designed to investigate the buckling behavior of a rectangular plate under compressive load. The rectangular plate was modeled and analyzed using the finite element analysis software ANSYS Workbench (academic 2023 R1). It simulates an Anti-Symmetric Angle-Ply composite plate with var...

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Main Author: Zhang, Hao
Other Authors: Chai Gin Boay
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2024
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Online Access:https://hdl.handle.net/10356/178550
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1785502024-06-29T16:49:57Z Finite element analysis of the buckling of rectangular composite plates in compression Zhang, Hao Chai Gin Boay School of Mechanical and Aerospace Engineering MGBCHAI@ntu.edu.sg Engineering Mechanical engineering Materials of construction This project is designed to investigate the buckling behavior of a rectangular plate under compressive load. The rectangular plate was modeled and analyzed using the finite element analysis software ANSYS Workbench (academic 2023 R1). It simulates an Anti-Symmetric Angle-Ply composite plate with various aspect ratios, stacking angles, and boundary conditions. The report analyzed the simulation results and determined the plate's coupling effects. The boundary conditions involved in the projects are simple support boundary conditions only. They are renamed as S1, S2, S3, and S4. Their purpose is to constrain the motion of the plate in the x and y directions. S1 constrained the movement in both directions, S2 limited the displacement in the y direction, S3 blocked the motion in the x direction, and S4 had no constraints. The stacking sequence of the composite plate varies from 2 to 8 plies, the stacking angle started from 0˚ and ended at 90˚ with an increment of 15˚. The ANSYS simulation showed that the rectangular composite plate in the S1 boundary condition has the relatively highest non-dimensional buckling force, and the bucking response for the plate in the remaining 3 boundary conditions depends on the aspect ratio and stacking angles. Therefore, the plate in the S1 boundary condition has the relatively lowest coupling effects among the 4 boundary conditions. In addition, the results revealed that the coupling effect is inverse-proportional to the number of plates, it decreases with the increase in plate number. Future improvements for this project include redesigning the ANSYS model or validating the results by applying it to other FEA software, such as ABAQUS and NX Nastran. Bachelor's degree 2024-06-26T00:17:20Z 2024-06-26T00:17:20Z 2024 Final Year Project (FYP) Zhang, H. (2024). Finite element analysis of the buckling of rectangular composite plates in compression. Final Year Project (FYP), Nanyang Technological University, Singapore. https://hdl.handle.net/10356/178550 https://hdl.handle.net/10356/178550 en B024 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
Mechanical engineering
Materials of construction
spellingShingle Engineering
Mechanical engineering
Materials of construction
Zhang, Hao
Finite element analysis of the buckling of rectangular composite plates in compression
description This project is designed to investigate the buckling behavior of a rectangular plate under compressive load. The rectangular plate was modeled and analyzed using the finite element analysis software ANSYS Workbench (academic 2023 R1). It simulates an Anti-Symmetric Angle-Ply composite plate with various aspect ratios, stacking angles, and boundary conditions. The report analyzed the simulation results and determined the plate's coupling effects. The boundary conditions involved in the projects are simple support boundary conditions only. They are renamed as S1, S2, S3, and S4. Their purpose is to constrain the motion of the plate in the x and y directions. S1 constrained the movement in both directions, S2 limited the displacement in the y direction, S3 blocked the motion in the x direction, and S4 had no constraints. The stacking sequence of the composite plate varies from 2 to 8 plies, the stacking angle started from 0˚ and ended at 90˚ with an increment of 15˚. The ANSYS simulation showed that the rectangular composite plate in the S1 boundary condition has the relatively highest non-dimensional buckling force, and the bucking response for the plate in the remaining 3 boundary conditions depends on the aspect ratio and stacking angles. Therefore, the plate in the S1 boundary condition has the relatively lowest coupling effects among the 4 boundary conditions. In addition, the results revealed that the coupling effect is inverse-proportional to the number of plates, it decreases with the increase in plate number. Future improvements for this project include redesigning the ANSYS model or validating the results by applying it to other FEA software, such as ABAQUS and NX Nastran.
author2 Chai Gin Boay
author_facet Chai Gin Boay
Zhang, Hao
format Final Year Project
author Zhang, Hao
author_sort Zhang, Hao
title Finite element analysis of the buckling of rectangular composite plates in compression
title_short Finite element analysis of the buckling of rectangular composite plates in compression
title_full Finite element analysis of the buckling of rectangular composite plates in compression
title_fullStr Finite element analysis of the buckling of rectangular composite plates in compression
title_full_unstemmed Finite element analysis of the buckling of rectangular composite plates in compression
title_sort finite element analysis of the buckling of rectangular composite plates in compression
publisher Nanyang Technological University
publishDate 2024
url https://hdl.handle.net/10356/178550
_version_ 1814047103889965056