Numerical analysis of fibre-bridging in perforated fibre metal laminate

Fibre-metal laminates are a new class of structural used in aerospace, which consists of fibre-reinforced prepegs, sandwiched between metal aluminum sheets. A numerical analysis of the fibre-bridging mechanism in fibre-metal laminates has been carried out using the boundary element and finite elemen...

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Bibliographic Details
Main Author: Chua, Yih Sheng.
Other Authors: Ang, Hock Eng
Format: Thesis
Published: 2008
Subjects:
Online Access:http://hdl.handle.net/10356/5657
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author Chua, Yih Sheng.
author2 Ang, Hock Eng
author_facet Ang, Hock Eng
Chua, Yih Sheng.
author_sort Chua, Yih Sheng.
collection NTU
description Fibre-metal laminates are a new class of structural used in aerospace, which consists of fibre-reinforced prepegs, sandwiched between metal aluminum sheets. A numerical analysis of the fibre-bridging mechanism in fibre-metal laminates has been carried out using the boundary element and finite element method. The fibre bridging stress and stress intensity factors was determined based on the fracture mechanics approach. The theory of linear elastic fracture mechanics, the formulation of the boundary integral equation with quarter-point crack-tip element and toughening mechanism in composite materials are also reviewed in this study. The effects of varying geometric parameters, the extent of bridging zone and the delamination shape between the prepeg and metal layers on the fibre bridging strength was also studied. The numerical analysis was extended to single perforated fibre-metal laminates and those containing multiple auxiliary holes was also performed. The numerical results obtained would be useful to obtain a better qualitative understanding of the crack-face bridging mechanism in fibre-metal laminates.
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spelling ntu-10356/56572023-03-11T17:05:53Z Numerical analysis of fibre-bridging in perforated fibre metal laminate Chua, Yih Sheng. Ang, Hock Eng School of Mechanical and Production Engineering DRNTU::Engineering::Aeronautical engineering::Materials of construction Fibre-metal laminates are a new class of structural used in aerospace, which consists of fibre-reinforced prepegs, sandwiched between metal aluminum sheets. A numerical analysis of the fibre-bridging mechanism in fibre-metal laminates has been carried out using the boundary element and finite element method. The fibre bridging stress and stress intensity factors was determined based on the fracture mechanics approach. The theory of linear elastic fracture mechanics, the formulation of the boundary integral equation with quarter-point crack-tip element and toughening mechanism in composite materials are also reviewed in this study. The effects of varying geometric parameters, the extent of bridging zone and the delamination shape between the prepeg and metal layers on the fibre bridging strength was also studied. The numerical analysis was extended to single perforated fibre-metal laminates and those containing multiple auxiliary holes was also performed. The numerical results obtained would be useful to obtain a better qualitative understanding of the crack-face bridging mechanism in fibre-metal laminates. Master of Engineering (MPE) 2008-09-17T10:55:57Z 2008-09-17T10:55:57Z 2000 2000 Thesis http://hdl.handle.net/10356/5657 Nanyang Technological University application/pdf
spellingShingle DRNTU::Engineering::Aeronautical engineering::Materials of construction
Chua, Yih Sheng.
Numerical analysis of fibre-bridging in perforated fibre metal laminate
title Numerical analysis of fibre-bridging in perforated fibre metal laminate
title_full Numerical analysis of fibre-bridging in perforated fibre metal laminate
title_fullStr Numerical analysis of fibre-bridging in perforated fibre metal laminate
title_full_unstemmed Numerical analysis of fibre-bridging in perforated fibre metal laminate
title_short Numerical analysis of fibre-bridging in perforated fibre metal laminate
title_sort numerical analysis of fibre bridging in perforated fibre metal laminate
topic DRNTU::Engineering::Aeronautical engineering::Materials of construction
url http://hdl.handle.net/10356/5657
work_keys_str_mv AT chuayihsheng numericalanalysisoffibrebridginginperforatedfibremetallaminate