Crushing behaviour of composite square honeycomb structure: a finite element analysis

Authors

  • Z. Ansari Structural Materials & Degradation Focus Group, Faculty of Mechanical Engineering, Universiti Malaysia Pahang, 26600 Pekan, Pahang, Malaysia
  • C.W. Tan Structural Materials & Degradation Focus Group, Faculty of Mechanical Engineering, Universiti Malaysia Pahang, 26600 Pekan, Pahang, Malaysia
  • M.R.M. Rejab Structural Materials & Degradation Focus Group, Faculty of Mechanical Engineering, Universiti Malaysia Pahang, 26600 Pekan, Pahang, Malaysia
  • D. Bachtiar Structural Materials & Degradation Focus Group, Faculty of Mechanical Engineering, Universiti Malaysia Pahang, 26600 Pekan, Pahang, Malaysia
  • J. Siregar Structural Materials & Degradation Focus Group, Faculty of Mechanical Engineering, Universiti Malaysia Pahang, 26600 Pekan, Pahang, Malaysia
  • M.Y.M. Zuhri Faculty of Engineering, Universiti Putra Malaysia, 43400 UPM Serdang, Selangor, Malaysia
  • N.S.D.M. Marzuki Structural Materials & Degradation Focus Group, Faculty of Mechanical Engineering, Universiti Malaysia Pahang, 26600 Pekan, Pahang, Malaysia

DOI:

https://doi.org/10.15282/jmes.11.2.2017.7.0241

Keywords:

Honeycomb square; crushing behavior; energy absorption.

Abstract

This paper investigates the compression properties of square honeycomb core materials based on glass fibre reinforced plastic. The objective of this project is to determine the failure strength and energy absorption of the square honeycomb structure and compare both crushing behaviours between the experimental and finite element simulations. Control specimen made from GFRP is prepared by using traditional hand lay-up technique and the mechanical properties are determined from the INSTRON Tensile Machine. In this study, the numerical simulation of the square honeycomb structure is analysed with the commercial software. In this simulation, the result obtained for maximum stress is 28.24MPa which is located at node 110451. Besides that, the energy absorption for finite element result and experimental result are 310.86 kJ and 282.17 kJ, respectively. The percentage of error is 9.23% which can be considered a good agreement between numerical simulation and experimental result. Lastly, the crushing behaviour between the finite element model and experimental model is slightly different to each other since the model in simulation is assumed to be the preferred structure, whereas the experimental model is imperfect in the geometric model.

References

Li M, Deng Z-q, Guo H-w, Liu R-q, Ding B-c. Optimizing crashworthiness design of square honeycomb structure. Journal of Central South University. 2014;21:912-9.

Wan Dalina WAD, Mariatti M, Mohd Ishak ZA, Mohamed AR. Comparison of properties of mwcnt/carbon fibre/ epoxy laminated composites prepared by solvent spraying method. International Journal of Automotive and Mechanical Engineering. 2014;10:1901-9.

Ravi Sankar H, Srikant RR, Vamsi Krishna P, Bhujanga Rao V, Bangaru Babu P. Estimation of the dynamic properties of epoxy glass fabric composites with natural rubber particle inclusions. International Journal of Automotive and Mechanical Engineering. 2013;7:968-80.

Karakoç A, Freund J. A statistical failure initiation model for honeycomb materials. Composite structures. 2013;95:154-62.

Nazirah ZS, Abdul Majid MS, Daud R. Effects of elevated temperatures on glass-reinforced epoxy pipes under multi-axial loadings. Journal of Mechanical Engineering and Sciences. 2016;10:1846-56.

Fairuz AM, Sapuan SM, Zainudin ES, Jaafar CNA. Effect of filler loading on mechanical properties of pultruded kenaf fibre reinforced vinyl ester composites. Journal of Mechanical Engineering and Sciences. 2016;10:1931-42.

Abdul Majid MS, Daud R, Afendi M, Amin NAM, Cheng EM, Gibson AG, et al. Stress-strain response modelling of glass fibre reinforced epoxy composite pipes under multiaxial loadings. Journal of Mechanical Engineering and Sciences. 2014;6:916-28.

Shen C, Lu G, Yu T. Dynamic behavior of graded honeycombs–a finite element study. Composite structures. 2013;98:282-93.

Asprone D, Auricchio F, Menna C, Morganti S, Prota A, Reali A. Statistical finite element analysis of the buckling behavior of honeycomb structures. Composite structures. 2013;105:240-55.

Arifin A, Abdullah S, Rafiquzzaman M, Zulkifli R, Wahab D. Failure characterisation in polymer matrix composite for un-notched and notched (open-hole) specimens under tension condition. Fibers and Polymers. 2014;15:1729-38.

Jones RM. Mechanics of composite materials: CRC press; 1998.

Sutherland L, Soares CG. Impact tests on woven-roving e-glass/polyester laminates. Composites Science and Technology. 1999;59:1553-67.

Kolawole MY, Aweda JO, Abdulkareem S. Archachatina marginata bio-shells as reinforcement material in metal matrix composites. International Journal of Automotive and Mechanical Engineering. 2017;14:4068-79.

Ahmed S, Ahsan A, Hasan M. Physico-mechanical properties of coir and jute fibre reinforced hybrid polyethylene composites. International Journal of Automotive and Mechanical Engineering. 2017;14:3927-37.

Fatchurrohman N, Sulaiman S, Sapuan SM, Ariffin MKA, Baharuddin BTHT. Analysis of a metal matrix composites automotive component. International Journal of Automotive and Mechanical Engineering. 2015;11:2531-40.

Gdoutos EE, Pilakoutas K, Rodopoulos C. Failure analysis of industrial composite materials: McGraw-Hill Professional; 2000.

Then YY, Ibrahim NA, Zainuddin N, Ariffin H, Wan Yunus WMZ, Abd Rahman MF. Effect of electron beam irradiation on the tensile properties of oil palm mesocarp fibre/poly(butylene succinate) biocomposites. International Journal of Automotive and Mechanical Engineering. 2014;10:2070-80.

Othman RN, Wilkinson AN. The impedance characterization of hybrid cnt-silica epoxy nanocomposites. International Journal of Automotive and Mechanical Engineering. 2014;10:1832-40.

Mohamad M, Marzuki HFA, Bakar SNA, Abdullah AN, Ubaidillah EAE, Abidin MFZ, et al. Effect of anodizing electrolyte for structural adhesives bonding study of aluminium-carbon laminates composites. International Journal of Automotive and Mechanical Engineering. 2014;10:2091-101.

Maleque MA, Radhi M, Rahman MM. Wear study of mg-sicp reinforcement aluminium metal matrix composite. Journal of Mechanical Engineering and Sciences. 2016;10:1758-64.

Kalpakjian S. Manufacturing engineering and technology ( 6th ed in si unit)2010.

Ahmad R, Ajer MR. Investigation of epoxy powder coated galvanized steel substrate through electrostatic powder coating system. International Journal of Automotive and Mechanical Engineering. 2015;11:2622-38.

Ismail AE, Che Abdul Aziz MA. Tensile strength of woven yarn kenaf fiber reinforced polyester composites. Journal of Mechanical Engineering and Sciences. 2015;9:1695-704.

Ibrahim MS, Sapuan SM, Faieza AA. Mechanical and thermal properties of composites from unsaturated polyester filled with oil palm ash. Journal of Mechanical Engineering and Sciences. 2012;2:133-47.

Hamdan S, Kiew KS, Rahman MR. Dielectric properties of maleic anhydride modified unsaturated polyester composites reinforced with chicken feather fibre. International Journal of Automotive and Mechanical Engineering. 2014;10:1971-9.

Lubin G. Handbook of composite materials. Van Nostrand Reinhold Co; 1982.

Hafizi ZM, Epaarachchi J, Lau KT. An investigation of acoustic emission signal attenuation for monitoring of progressive failure in fiberglass reinforced composite laminates. International Journal of Automotive and Mechanical Engineering. 2013;8:1442-56.

Jeffrey KJT, Tarlochan F, Rahman MM. Residual strength of chop strand mats glass fiber/epoxy composite structures: Effect of temperature and water absorption. International Journal of Automotive and Mechanical Engineering. 2011;4:504-19.

Chan WT. The effects of fibre volume fraction of composite plate: Universiti Malaysia Pahang; 2007.

Tawfik S, Tan X, Ozbay S, Armanios E. Anticlastic stability modeling for cross-ply composites. Journal of Composite Materials. 2007;41:1325-38.

Rejab M, Cantwell W. The mechanical behaviour of corrugated-core sandwich panels. Composites Part B: Engineering. 2013;47:267-77.

Hibbitt K. Abaqus: User's manual: Version 6.13: Hibbitt. Karlsson & Sorensen, Incorporated. 2013.

Rejab M, Ushijima K, Cantwell W. The shear response of lightweight corrugated core structures. Journal of Composite Materials. 2013:0021998313514086.

Zuhri MYM, Guan ZW, Cantwell WJ. The mechanical properties of natural fibre based honeycomb core materials. Composites Part B: Engineering. 2014;58:1-9.

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Published

2017-06-30

How to Cite

[1]
Z. Ansari, “Crushing behaviour of composite square honeycomb structure: a finite element analysis”, J. Mech. Eng. Sci., vol. 11, no. 2, pp. 2637–2649, Jun. 2017.

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