Please use this identifier to cite or link to this item: http://hdl.handle.net/11452/30158
Title: Finite-element analysis of EPP foam core/self-reinforced PP sandwich structures
Authors: Türkoğlu, İbrahim Kürşad
Yücel, Can
Bursa Uludağ Üniversitesi/Mühendislik Fakültesi/Otomotiv Mühendisliği Bölümü.
0000-0002-5679-313X
0000-0002-8720-7594
Güçlü, Harun
Yazıcı, Murat
M-4741-2017
ABI-3125-2020
Q-8738-2018
57191191009
7007162323
Keywords: ABAQUS
Bending (deformation)
Bending dies
Composite beams and girders
Compression testing
Elastoplasticity
Foams
Honeycomb structures
Plastic deformation
Plastics industry
Polypropylenes
Reinforced plastics
Sandwich structures
Absorption performance
Crushable foam materials
Elastic-plastic deformation
Foam core sandwiches
Self-reinforced polypropylenes
Thermoplastic composite
Three-dimensional (3D) space
Three-point-bending experiments
Finite element method
Issue Date: 22-Dec-2020
Publisher: Ice Publishing
Citation: Güçlü, H. vd. (2020). "Finite-element analysis of EPP foam core/self-reinforced PP sandwich structures". Emerging Materials Research, 9(4), 1250-1257.
Abstract: In this study, fully recyclable and elastic-plastic deformable sandwich panels were developed by considering the mass production requirements, as well as the lightweighting needs of the automotive industry. Expanded polypropylene (EPP) foam core and self-reinforced polypropylene (PP) thermoplastic composite face sheets were selected to produce sandwich panels. Three-point bending experiments were performed to obtain the flexural behavior of the sandwich panels. Finite-element analysis (FEA) of the sandwich beams was carried out and confirmed by experimental results. Three different EPP foam cores with densities of 65.7, 36.5 and 27.0 kg/m(3) were used. The FEA models were built in the Abaqus commercial software in three-dimensional (3D) space, and analyses were performed using 3D elements. The crushable foam material model was selected for FEA from the Abaqus material model database to obtain the best correlation with the foam compression test results. The force-displacement results of the three-point bending FEA results excellently correlated with the experiments. In three-point bending experiments of the sandwich panels, elastic-plastic deformation of the core with indentation failure was observed. The lowest-density foam core sandwich beam showed the highest deformation and energy absorption performance. Also, deflection recovery was observed after load removal for all sandwiches.
URI: https://doi.org/10.1680/Jemmr.19.00194
https://www.icevirtuallibrary.com/doi/10.1680/jemmr.19.00194
http://hdl.handle.net/11452/30158
ISSN: 2046-0147
2046-0155
Appears in Collections:Scopus
Web of Science

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