Loading Rate Effect on Flexural and Indentation Behaviour of Foam Core Composite Sandwich Panel

Authors

  • Azwan S. Centre for Composites (CfC), Faculty of Mechanical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor Malaysia
  • Yazid Yahya Centre for Composites (CfC), Faculty of Mechanical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor Malaysia
  • B. Abdi Centre for Composites (CfC), Faculty of Mechanical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor Malaysia
  • Amran Ayob Centre for Composites (CfC), Faculty of Mechanical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor Malaysia

DOI:

https://doi.org/10.11113/jt.v71.3737

Keywords:

Loading rate, flexural, indentation, energy absorption, sandwich panel

Abstract

The present study focuses on the flexural and the indentation behaviour of foam core sandwich panel subject to three point bending and indentation loading at different loading rates. The load-deflection, stress-deflection responses and energy absorption properties of foam core sandwich panel are determined experimentally. The foam core sandwich panel was fabricated using vacuum infusion process. The sandwich structure consists of chopped strand mat fibreglass skins and polyurethane foam core. The flexural and the indentation tests were conducted using Instron Universal Testing machine. It was found that loading rate influences the flexural and the indentation behaviours of foam core sandwich panel. By increasing the loading rate, the stiffness, strength and energy absorption of flexural and indentation of these structures were increased.

 

References

E.A. Flores-Johnson, Q.M. Li. 2011. Experimental study of the indentation of sandwich panels with carbon fiber-reinforced polymer facesheets and polymeric foam core. Compos. Part B-Eng. 42(5): 1212–1219.

A. Mostafa, K. Shankar, E.V. Morozov. 2013. Insight into the shear behavior of composite sandwich panels with foam core. Mater. Des. 50: 92–101.

A. Russo. B. Zuccarello. 2007. Experimental and numerical evaluation of the mechanical behavior of GFRP sandwich panels. Compos. Struct. 81(4): 575–586.

J. Wang, A.M. Waas, H. Wang. 2013. Experimental and numerical study on th elow-velocity impact behavior of foam-core sandwich panels. Compos. Struct. 96: 298–311.

B. Abdi, S.S.R. Koloor, M.R. Abdullah, M.Y. bin Yahya. 2012. Effect of strain rate on flexural behavior of composite sandwich panel. Appl. Mech. Mater. 229: 766–770.

A. Chemami, K. Bey, J. Gilgert, Z. Azari. 2012. Behavior of composite sandwich foam-laminated glass/epoxy under solicitation static and fatigue. Compos. Part B-Eng. 43(3): 1178–1184.

M. Bîrsan, T. Sadowski, L. Marsavina, E. Linul, D. Pietras. 2013. Mechanical behavior of sandwich composite beams made of foams and functinally graded materials. Int. J. Solids Struct. 50(3–4): 519–530.

ASTM C365/C365M-05. Standard test method for flatwise compressive properties of sandwich cores. Philadelphia, PA. American Society for Testing and Materials.

ASTM D790-10.Standard test methods for flexural properties of unreinforced and reinforced plastics and electrical insulating materials. Philadelphia, PA. American Society for Testing and Materials.

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Published

2014-11-27

How to Cite

Loading Rate Effect on Flexural and Indentation Behaviour of Foam Core Composite Sandwich Panel. (2014). Jurnal Teknologi (Sciences & Engineering), 71(2). https://doi.org/10.11113/jt.v71.3737