Structural Response of Polyethylene Foam-Based Sandwich Panels Subjected to Edgewise Compression

This study analyzes the mechanical behavior of low density polyethylene foam core sandwich panels subjected to edgewise compression. In order to monitor panel response to buckling, strains generated in the facesheets and overall out-of-plane deformations are measured with strain gages and projection...

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Main Authors: Luciano Lamberti, Caterina Casavola, Antonio Boccaccio, Carmine Pappalettere
Format: Article
Language:English
Published: MDPI AG 2013-10-01
Series:Materials
Subjects:
Online Access:http://www.mdpi.com/1996-1944/6/10/4545
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spelling doaj-21dd1857111c4d87957693f6a1c6376c2020-11-24T23:00:37ZengMDPI AGMaterials1996-19442013-10-016104545456410.3390/ma6104545Structural Response of Polyethylene Foam-Based Sandwich Panels Subjected to Edgewise CompressionLuciano LambertiCaterina CasavolaAntonio BoccaccioCarmine PappalettereThis study analyzes the mechanical behavior of low density polyethylene foam core sandwich panels subjected to edgewise compression. In order to monitor panel response to buckling, strains generated in the facesheets and overall out-of-plane deformations are measured with strain gages and projection moiré, respectively. A finite element (FE) model simulating the experimental test is developed. Numerical results are compared with moiré measurements. After having been validated against experimental evidence, the FE model is parameterized, and a trade study is carried out to investigate to what extent the structural response of the panel depends on the sandwich wall construction and facesheet/core interface defects. The projection moiré set-up utilized in this research is able to capture the sudden and very localized buckling phenomena occurring under edgewise compression of foam-based sandwich panels. Results of parametric FE analyses indicate that, if the total thickness of the sandwich wall is fixed, including thicker facesheets in the laminate yields a larger deflection of the panel that becomes more sensitive to buckling. Furthermore, the mechanical response of the foam sandwich panel is found to be rather insensitive to the level of waviness of core-facesheet interfaces.http://www.mdpi.com/1996-1944/6/10/4545foam-based coresandwich panelsedgewise compressionbucklingout-of-plane displacementprojection moirénonlinear finite element analysisfacesheet-to-core thickness ratiofacesheet/core interface waviness
collection DOAJ
language English
format Article
sources DOAJ
author Luciano Lamberti
Caterina Casavola
Antonio Boccaccio
Carmine Pappalettere
spellingShingle Luciano Lamberti
Caterina Casavola
Antonio Boccaccio
Carmine Pappalettere
Structural Response of Polyethylene Foam-Based Sandwich Panels Subjected to Edgewise Compression
Materials
foam-based coresandwich panels
edgewise compression
buckling
out-of-plane displacement
projection moiré
nonlinear finite element analysis
facesheet-to-core thickness ratio
facesheet/core interface waviness
author_facet Luciano Lamberti
Caterina Casavola
Antonio Boccaccio
Carmine Pappalettere
author_sort Luciano Lamberti
title Structural Response of Polyethylene Foam-Based Sandwich Panels Subjected to Edgewise Compression
title_short Structural Response of Polyethylene Foam-Based Sandwich Panels Subjected to Edgewise Compression
title_full Structural Response of Polyethylene Foam-Based Sandwich Panels Subjected to Edgewise Compression
title_fullStr Structural Response of Polyethylene Foam-Based Sandwich Panels Subjected to Edgewise Compression
title_full_unstemmed Structural Response of Polyethylene Foam-Based Sandwich Panels Subjected to Edgewise Compression
title_sort structural response of polyethylene foam-based sandwich panels subjected to edgewise compression
publisher MDPI AG
series Materials
issn 1996-1944
publishDate 2013-10-01
description This study analyzes the mechanical behavior of low density polyethylene foam core sandwich panels subjected to edgewise compression. In order to monitor panel response to buckling, strains generated in the facesheets and overall out-of-plane deformations are measured with strain gages and projection moiré, respectively. A finite element (FE) model simulating the experimental test is developed. Numerical results are compared with moiré measurements. After having been validated against experimental evidence, the FE model is parameterized, and a trade study is carried out to investigate to what extent the structural response of the panel depends on the sandwich wall construction and facesheet/core interface defects. The projection moiré set-up utilized in this research is able to capture the sudden and very localized buckling phenomena occurring under edgewise compression of foam-based sandwich panels. Results of parametric FE analyses indicate that, if the total thickness of the sandwich wall is fixed, including thicker facesheets in the laminate yields a larger deflection of the panel that becomes more sensitive to buckling. Furthermore, the mechanical response of the foam sandwich panel is found to be rather insensitive to the level of waviness of core-facesheet interfaces.
topic foam-based coresandwich panels
edgewise compression
buckling
out-of-plane displacement
projection moiré
nonlinear finite element analysis
facesheet-to-core thickness ratio
facesheet/core interface waviness
url http://www.mdpi.com/1996-1944/6/10/4545
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