Mechanical behaviour of pin-reinforced foam core sandwich panels subjected to low impact loading

As a light structure, composite sandwich panels are distinguished by their significant bending stiffness that is rapidly used in the manufacture of aircraft bodies. This study focuses on the mechanical behaviour of through-thickness polymer, pin-reinforced foam core sandwich panels subjected to inde...

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Main Authors: Nejad, Ali Farokhi, Koloor, Seyed Saeid Rahimian, Syed Hamzah, Syed Mohd. Saiful Azwan, Yahya, Mohd. Yazid
Format: Article
Language:English
Published: MDPI 2021
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Online Access:http://eprints.utm.my/id/eprint/97565/1/MohdYazidYahya2021_MechanicalBehaviourofPinReinforcedFoam.pdf
http://eprints.utm.my/id/eprint/97565/
http://dx.doi.org/10.3390/polym13213627
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spelling my.utm.975652022-10-18T02:21:26Z http://eprints.utm.my/id/eprint/97565/ Mechanical behaviour of pin-reinforced foam core sandwich panels subjected to low impact loading Nejad, Ali Farokhi Koloor, Seyed Saeid Rahimian Syed Hamzah, Syed Mohd. Saiful Azwan Yahya, Mohd. Yazid TJ Mechanical engineering and machinery As a light structure, composite sandwich panels are distinguished by their significant bending stiffness that is rapidly used in the manufacture of aircraft bodies. This study focuses on the mechanical behaviour of through-thickness polymer, pin-reinforced foam core sandwich panels subjected to indentation and low impact loading. Experimental and computational approaches are used to study the global and internal behaviour of the sandwich panel. The samples for experimental testing were made from glass/polyester laminates as the face sheets and polyurethane foam as the foam core. To further reinforce the samples against bending, different sizes of polymeric pins were implemented on the sandwich panels. The sandwich panel was fabricated using the vacuum infusion process. Using the experimental data, a finite element model of the sample was generated in LS-DYNA software, and the effect of pin size and loading rate were examined. Results of the simulation were validated through a proper prediction compared to the test data. The results of the study show that using polymeric pins, the flexural strength of the panel significantly increased under impact loading. In addition, the impact resistance of the pin-reinforced foam core panel increased up to 20%. Moreover, the size of pins has a significant influence on the flexural behaviour while the sample was under a moderate strain rate. To design an optimum pin-reinforced sandwich panel a “design of experiment model” was generated to predict energy absorption and the maximum peak load of proposed sandwich panels. The best design of the panel is recommended with 1.8 mm face sheet thickness and 5 mm pins diameter. MDPI 2021 Article PeerReviewed application/pdf en http://eprints.utm.my/id/eprint/97565/1/MohdYazidYahya2021_MechanicalBehaviourofPinReinforcedFoam.pdf Nejad, Ali Farokhi and Koloor, Seyed Saeid Rahimian and Syed Hamzah, Syed Mohd. Saiful Azwan and Yahya, Mohd. Yazid (2021) Mechanical behaviour of pin-reinforced foam core sandwich panels subjected to low impact loading. Polymers, 13 (21). pp. 1-17. ISSN 2073-4360 http://dx.doi.org/10.3390/polym13213627 DOI : 10.3390/polym13213627
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
language English
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Nejad, Ali Farokhi
Koloor, Seyed Saeid Rahimian
Syed Hamzah, Syed Mohd. Saiful Azwan
Yahya, Mohd. Yazid
Mechanical behaviour of pin-reinforced foam core sandwich panels subjected to low impact loading
description As a light structure, composite sandwich panels are distinguished by their significant bending stiffness that is rapidly used in the manufacture of aircraft bodies. This study focuses on the mechanical behaviour of through-thickness polymer, pin-reinforced foam core sandwich panels subjected to indentation and low impact loading. Experimental and computational approaches are used to study the global and internal behaviour of the sandwich panel. The samples for experimental testing were made from glass/polyester laminates as the face sheets and polyurethane foam as the foam core. To further reinforce the samples against bending, different sizes of polymeric pins were implemented on the sandwich panels. The sandwich panel was fabricated using the vacuum infusion process. Using the experimental data, a finite element model of the sample was generated in LS-DYNA software, and the effect of pin size and loading rate were examined. Results of the simulation were validated through a proper prediction compared to the test data. The results of the study show that using polymeric pins, the flexural strength of the panel significantly increased under impact loading. In addition, the impact resistance of the pin-reinforced foam core panel increased up to 20%. Moreover, the size of pins has a significant influence on the flexural behaviour while the sample was under a moderate strain rate. To design an optimum pin-reinforced sandwich panel a “design of experiment model” was generated to predict energy absorption and the maximum peak load of proposed sandwich panels. The best design of the panel is recommended with 1.8 mm face sheet thickness and 5 mm pins diameter.
format Article
author Nejad, Ali Farokhi
Koloor, Seyed Saeid Rahimian
Syed Hamzah, Syed Mohd. Saiful Azwan
Yahya, Mohd. Yazid
author_facet Nejad, Ali Farokhi
Koloor, Seyed Saeid Rahimian
Syed Hamzah, Syed Mohd. Saiful Azwan
Yahya, Mohd. Yazid
author_sort Nejad, Ali Farokhi
title Mechanical behaviour of pin-reinforced foam core sandwich panels subjected to low impact loading
title_short Mechanical behaviour of pin-reinforced foam core sandwich panels subjected to low impact loading
title_full Mechanical behaviour of pin-reinforced foam core sandwich panels subjected to low impact loading
title_fullStr Mechanical behaviour of pin-reinforced foam core sandwich panels subjected to low impact loading
title_full_unstemmed Mechanical behaviour of pin-reinforced foam core sandwich panels subjected to low impact loading
title_sort mechanical behaviour of pin-reinforced foam core sandwich panels subjected to low impact loading
publisher MDPI
publishDate 2021
url http://eprints.utm.my/id/eprint/97565/1/MohdYazidYahya2021_MechanicalBehaviourofPinReinforcedFoam.pdf
http://eprints.utm.my/id/eprint/97565/
http://dx.doi.org/10.3390/polym13213627
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score 13.160551