Biaxial testing of adhesively bonded composite joints

Debonding has been noted as the main cause of failure in bonded composite assemblies and there have been many studies to characterize the failure models surrounding the complex nature of adhesive bond failure. In this study, the author has fabricated and recycled Glass Fiber Reinforced Polymer (GF...

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Main Author: Yap, Jeanette Xin Yi
Other Authors: Sridhar Idapalapati
Format: Final Year Project
Language:English
Published: 2018
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Online Access:http://hdl.handle.net/10356/74876
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-748762023-03-04T18:34:43Z Biaxial testing of adhesively bonded composite joints Yap, Jeanette Xin Yi Sridhar Idapalapati School of Mechanical and Aerospace Engineering DRNTU::Engineering Debonding has been noted as the main cause of failure in bonded composite assemblies and there have been many studies to characterize the failure models surrounding the complex nature of adhesive bond failure. In this study, the author has fabricated and recycled Glass Fiber Reinforced Polymer (GFRP) specimens to be joined using epoxy adhesive to perform mixed-mode biaxial loading experiments using a modified Arcan Setup. Three types of adhesive joint profiles were used to test and compare the fracture characteristics of the specimens. ABAQUS® finite element analysis software was then used to simulate the experimental measurements of load-displacement to determine a suitable failure model that could fit the fracture mechanics of the debonding of the specimens through the use of cohesive elements and traction-separation law. It was determined that the quadratic nominal stress failure criterion fitted with power law damage evolution was suitable for the straight profile samples. For the rectangle profile, the failure criterion was only suitable for very low loading angles, however the Benzeggagh and Kenane (BK) mixed mode damage evolution criterion was able to predict crack patterns which the power law damage evolution was not able to. The failure criterion did not fit well for the triangle profile as most stresses were either over or under predicted by both damage evolution criterions. However, for loading angles at 60° and 75°, the power law damage evolution was able to predict peak loads. For the straight and rectangle designs, it was noted that the fracture energies predicted by the failure criterion was suitable for loading angles below 45°. For the triangle profile, the fracture energy was suitable for loading angles at 0°, 15° and 60°. Bachelor of Engineering (Mechanical Engineering) 2018-05-24T07:29:21Z 2018-05-24T07:29:21Z 2018 Final Year Project (FYP) http://hdl.handle.net/10356/74876 en Nanyang Technological University 114 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
spellingShingle DRNTU::Engineering
Yap, Jeanette Xin Yi
Biaxial testing of adhesively bonded composite joints
description Debonding has been noted as the main cause of failure in bonded composite assemblies and there have been many studies to characterize the failure models surrounding the complex nature of adhesive bond failure. In this study, the author has fabricated and recycled Glass Fiber Reinforced Polymer (GFRP) specimens to be joined using epoxy adhesive to perform mixed-mode biaxial loading experiments using a modified Arcan Setup. Three types of adhesive joint profiles were used to test and compare the fracture characteristics of the specimens. ABAQUS® finite element analysis software was then used to simulate the experimental measurements of load-displacement to determine a suitable failure model that could fit the fracture mechanics of the debonding of the specimens through the use of cohesive elements and traction-separation law. It was determined that the quadratic nominal stress failure criterion fitted with power law damage evolution was suitable for the straight profile samples. For the rectangle profile, the failure criterion was only suitable for very low loading angles, however the Benzeggagh and Kenane (BK) mixed mode damage evolution criterion was able to predict crack patterns which the power law damage evolution was not able to. The failure criterion did not fit well for the triangle profile as most stresses were either over or under predicted by both damage evolution criterions. However, for loading angles at 60° and 75°, the power law damage evolution was able to predict peak loads. For the straight and rectangle designs, it was noted that the fracture energies predicted by the failure criterion was suitable for loading angles below 45°. For the triangle profile, the fracture energy was suitable for loading angles at 0°, 15° and 60°.
author2 Sridhar Idapalapati
author_facet Sridhar Idapalapati
Yap, Jeanette Xin Yi
format Final Year Project
author Yap, Jeanette Xin Yi
author_sort Yap, Jeanette Xin Yi
title Biaxial testing of adhesively bonded composite joints
title_short Biaxial testing of adhesively bonded composite joints
title_full Biaxial testing of adhesively bonded composite joints
title_fullStr Biaxial testing of adhesively bonded composite joints
title_full_unstemmed Biaxial testing of adhesively bonded composite joints
title_sort biaxial testing of adhesively bonded composite joints
publishDate 2018
url http://hdl.handle.net/10356/74876
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