Biaxial failure response of composite laminates

In this report, two sets of experiments are conducted. The first is biaxial testing on cruciform shaped GFRP composite laminates and the second is tensile testing on Arcan test specimens. The biaxial test aims at comparing the axial and transverse stresses under biaxial testing. The samples have dif...

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Main Author: Nayar, Dhruv
Other Authors: Sridhar Idapalapati
Format: Final Year Project
Language:English
Published: 2015
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Online Access:http://hdl.handle.net/10356/65124
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-651242023-03-04T18:39:43Z Biaxial failure response of composite laminates Nayar, Dhruv Sridhar Idapalapati School of Mechanical and Aerospace Engineering DRNTU::Engineering::Mechanical engineering In this report, two sets of experiments are conducted. The first is biaxial testing on cruciform shaped GFRP composite laminates and the second is tensile testing on Arcan test specimens. The biaxial test aims at comparing the axial and transverse stresses under biaxial testing. The samples have different crack sizes and orientations. The tests are carried out on a new INSTRON machine. The Arcan tests aim at calculating the critical fracture toughness for modes I and II. The Arcan test jig is selected as this setup allows the extracting of fracture properties in various modes using only one shape and size of the specimen. The preparation methods for both sets of samples are described along with the curing process and curing cycles. The experiment results and data are tabulated and analyzed in detail. Finally, recommendations and scope for improvements have been highlighted. Finite element simulations using ABAQUS will also be used to obtain geometrical factors used in the calculation of the critical fracture toughness. Load-displacement curves, among other graph comparisons, are also included in the report. Bachelor of Engineering (Mechanical Engineering) 2015-06-15T03:26:33Z 2015-06-15T03:26:33Z 2015 2015 Final Year Project (FYP) http://hdl.handle.net/10356/65124 en Nanyang Technological University 101 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::Mechanical engineering
spellingShingle DRNTU::Engineering::Mechanical engineering
Nayar, Dhruv
Biaxial failure response of composite laminates
description In this report, two sets of experiments are conducted. The first is biaxial testing on cruciform shaped GFRP composite laminates and the second is tensile testing on Arcan test specimens. The biaxial test aims at comparing the axial and transverse stresses under biaxial testing. The samples have different crack sizes and orientations. The tests are carried out on a new INSTRON machine. The Arcan tests aim at calculating the critical fracture toughness for modes I and II. The Arcan test jig is selected as this setup allows the extracting of fracture properties in various modes using only one shape and size of the specimen. The preparation methods for both sets of samples are described along with the curing process and curing cycles. The experiment results and data are tabulated and analyzed in detail. Finally, recommendations and scope for improvements have been highlighted. Finite element simulations using ABAQUS will also be used to obtain geometrical factors used in the calculation of the critical fracture toughness. Load-displacement curves, among other graph comparisons, are also included in the report.
author2 Sridhar Idapalapati
author_facet Sridhar Idapalapati
Nayar, Dhruv
format Final Year Project
author Nayar, Dhruv
author_sort Nayar, Dhruv
title Biaxial failure response of composite laminates
title_short Biaxial failure response of composite laminates
title_full Biaxial failure response of composite laminates
title_fullStr Biaxial failure response of composite laminates
title_full_unstemmed Biaxial failure response of composite laminates
title_sort biaxial failure response of composite laminates
publishDate 2015
url http://hdl.handle.net/10356/65124
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