Study of zero Poisson’s ratio honeycomb composite structure
Honeycomb sandwich core structures are generally well known for its light weight potential, high stiffness and high strength to weight ratio which are important for acoustic, aerospace, automotive and construction applications. There were a few proposed cellular designs to maximise the mechanical an...
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sg-ntu-dr.10356-783862023-03-04T15:39:46Z Study of zero Poisson’s ratio honeycomb composite structure Chia, Yingxue Huang Yizhong Song Xu School of Materials Science and Engineering A*STAR Singapore Institute of Manufacturing Technology DRNTU::Engineering::Materials::Material testing and characterization Honeycomb sandwich core structures are generally well known for its light weight potential, high stiffness and high strength to weight ratio which are important for acoustic, aerospace, automotive and construction applications. There were a few proposed cellular designs to maximise the mechanical and acoustical properties to fit the desired product shapes, but in this study, zero Poisson’s ratio honeycomb was chosen, and a prototype consisting of aluminium and polyester was subsequently handcrafted. By using zero Poisson’s ratio honeycomb structure, it may relieve problems of fitting into “out of plane” structures into the desired product shape, allowing the honeycomb sandwich panels to wrap around 2D curved surfaces without geometric trimming and comprising mechanical properties. The honeycomb core prototype’s dimensions were decided based on literature review, to produce a sturdy structure suitable for aircraft interior and fuselage. Bachelor of Engineering (Materials Engineering) 2019-06-19T06:30:33Z 2019-06-19T06:30:33Z 2019 Final Year Project (FYP) http://hdl.handle.net/10356/78386 en Nanyang Technological University 33 p. application/pdf |
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DRNTU::Engineering::Materials::Material testing and characterization Chia, Yingxue Study of zero Poisson’s ratio honeycomb composite structure |
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Honeycomb sandwich core structures are generally well known for its light weight potential, high stiffness and high strength to weight ratio which are important for acoustic, aerospace, automotive and construction applications. There were a few proposed cellular designs to maximise the mechanical and acoustical properties to fit the desired product shapes, but in this study, zero Poisson’s ratio honeycomb was chosen, and a prototype consisting of aluminium and polyester was subsequently handcrafted. By using zero Poisson’s ratio honeycomb structure, it may relieve problems of fitting into “out of plane” structures into the desired product shape, allowing the honeycomb sandwich panels to wrap around 2D curved surfaces without geometric trimming and comprising mechanical properties. The honeycomb core prototype’s dimensions were decided based on literature review, to produce a sturdy structure suitable for aircraft interior and fuselage. |
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Huang Yizhong |
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Huang Yizhong Chia, Yingxue |
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Final Year Project |
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Chia, Yingxue |
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Chia, Yingxue |
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Study of zero Poisson’s ratio honeycomb composite structure |
title_short |
Study of zero Poisson’s ratio honeycomb composite structure |
title_full |
Study of zero Poisson’s ratio honeycomb composite structure |
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Study of zero Poisson’s ratio honeycomb composite structure |
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Study of zero Poisson’s ratio honeycomb composite structure |
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study of zero poisson’s ratio honeycomb composite structure |
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2019 |
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http://hdl.handle.net/10356/78386 |
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