Assessing the impact resistance and damage tolerance of Aluminium composite fibre metal laminates under low velocity impact test

Authors

  • Mohd Fadhil Rani Faculty of Engineering and Technology, DRB-HICOM University of Automotive Malaysia, 26607 Pekan, Pahang, Malaysia
  • M. R. M. Rejab Faculty of Mechanical and Automotive Engineering Technology, Universiti Malaysia Pahang Al-Sultan Abdullah, 26600 Pekan, Malaysia
  • N. Ab. Razak Faculty of Mechanical and Automotive Engineering Technology, Universiti Malaysia Pahang Al-Sultan Abdullah, 26600 Pekan, Malaysia
  • M. I. Ibrahim Faculty of Engineering and Technology, DRB-HICOM University of Automotive Malaysia, 26607 Pekan, Pahang, Malaysia
  • M. Z. Azir Faculty of Engineering and Technology, DRB-HICOM University of Automotive Malaysia, 26607 Pekan, Pahang, Malaysia
  • Z. Zaulkafilai Faculty of Engineering and Technology, DRB-HICOM University of Automotive Malaysia, 26607 Pekan, Pahang, Malaysia

DOI:

https://doi.org/10.15282/jmes.19.3.2025.3.0841

Keywords:

Fibre metal laminate, Low velocity impact test, CFRP, GFRP, SRPP

Abstract

The automotive industry requires materials that are light in weight to enhance fuel efficiency while optimizing safety standards alongside having a high impact resistance to improve the vehicle's overall safety features. This study focuses on evaluating the low velocity impact performance of fibre metal laminates (FMLs) with different configurations to identify the most suitable crash resistant structures for vehicles. Five FML configurations were fabricated using 2024-T3 aluminum with CFRP (B2), GFRP (B1), SRPP (B3) and hybrid combinations consist of CFRP-GFRP (B4) and SRPP-GFRP (B5) in 3/2 layered structures that were tested under low-velocity impact at 2.7-4.5 m/s using drop-weight testing with force, displacement and energy absorption measurements. B5 recorded the highest impact force of 13827.1 N due to the synergistic bonding of thermoplastic SRPP and the GFRP layer. B1 exhibited the best energy absorption of 86.4 J outperforming other configurations by 10% because of the glass fibre's strain-to-failure characteristics which allows for significant plastic deformation. B2 lagged in both energy absorption and force at 78.5 J and 11476.2 N respectively due to the brittleness of the carbon fibre. The ranking for energy absorption was B1 > B4 > B2 > B5 > B3 with all configurations showing proportional increases in strength with velocity. Configuration B5 composed of hybrid SRPP-GFRP demonstrated the best impact resistance outperforming CFRP systems by 20.5% in force resistance, while GFRP-based FMLs (B1) showed better energy absorption at 86.4 J which is critical for managing crash energy thus illustrating that the selection of materials relies on the designated zone of an automobile meant to endure a collision, prioritizing either force resistance or energy dissipation.

References

[1] E. Haq, A. Saifullah, A. Habib, A. Y. M. A. Azim, S. Alimuzzaman, H. N. Dhakal, et al., “Improved mechanical properties of environmentally friendly jute fibre reinforced metal laminate sandwich composite through enhanced interface,” Heliyon, vol. 10, no. 2, p. e24345, 2024.

[2] A. B. Nia, L. Xin, M. Y. Yahya, A. Ayob, A. F. Nejad, S. S. R. Koloor, et al., “Failure of glass fibre-reinforced polypropylene metal laminate subjected to close-range explosion,” Polymers (Basel), vol. 12, no. 9, p. 2139, 2020.

[3] N. L. Feng, S. D. Malingam, C. W. Ping, ”Mechanical characterisation of kenaf/PALF reinforced composite-metal laminates: Effects of hybridisation and weaving architectures,” Journal of Reinforced Plastics and Composites, vol. 40, no. 5-6, pp. 193-205, 2021.

[4] Q. Ma, M. R. M. Rejab, N. A. Alang, M. M. Hanon, B. Yang, H. Hu, et al., “Crashworthiness performance of sandwich panel with self-reinforced polypropylene (SRPP) and carbon fiber-reinforced plastic (CFRP) spherical-roof contoured cores,” in Thin-Walled Composite Protective Structures for Crashworthiness Applications: Recent Advances and Future Developments, pp. 1–12, 2023.

[5] G. H. Payeganeh, F. Ashenai Ghasemi, K. Malekzadeh, “Dynamic response of fiber-metal laminates (FMLs) subjected to low-velocity impact,” Thin-Walled Structures, vol. 48, no. 1, pp. 62–70, 2010.

[6] Z. Asaee, F. Taheri, “Experimental and numerical investigation into the influence of stacking sequence on the low-velocity impact response of new 3D FMLs,” Composite Structures, vol. 140, pp. 136–146, 2016.

[7] A. Salve, R. Kulkarni, A. Mache, “A review: Fiber metal laminates (FML’s)—Manufacturing, test methods and numerical modeling,” International Journal of Engineering Technology and Sciences, vol. 6, pp. 1–12, 2016.

[8] S. Dariushi, S. Farahmandnia, A. M. Rezadoust, “An experimental investigation on infusion time and strength of fiber metal laminates made by vacuum infusion process,” Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications, vol. 235, no. 10, pp. 1800–1808, 2021.

[9] M. Safari, M. Salamat-Talab, A. Abdollahzade, A. Akhavan-Safar, L. F. M. da Silva, “Experimental investigation, statistical modeling and multi-objective optimization of creep age forming of fiber metal laminates,” Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications, vol. 234, no. 11, pp. 1389–1398, 2020.

[10] M. F. Rani, M. R. M. Mat Rejab, M. I. Ibrahim, N. K. Romli, “Mechanical characterization of 3/2 fibre metal laminate materials,” Journal of Mechanical Engineering and Sciences, vol. 17, no. 4, pp. 9753–9763, 2023.

[11] P. Jakubczak, M. Droździel, P. Podolak, J. Pernas-Sánchez, “Experimental investigation on the low velocity impact response of fibre foam metal laminates,” Materials, vol. 14, no. 19, p. 5510, 2021.

[12] K. Jin, K. Chen, X. Luo, J. Tao, “Fatigue crack growth and delamination mechanisms of Ti/CFRP fibre metal laminates at high temperatures,” Fatigue and Fracture of Engineering Materials and Structures, vol. 43, no. 5, pp. 1115–1125, 2020.

[13] L. M. G. Vieira, Y. Dobah, J. C. Dos Santos, T. H. Panzera, J. C. Campos Rubio, F. Scarpa, “Impact properties of novel natural fibre metal laminated composite materials,” Applied Sciences, vol. 12, no. 4, p. 1869, 2022.

[14] Z. Xie, W. Zhao, X. Wang, J. Hang, X. Yue, X. Zhou, “Low-velocity impact behaviour of titanium honeycomb sandwich structures,” Journal of Sandwich Structures and Materials, vol. 20, no. 8, pp. 1009–1027, 2018.

[15] Z. Li, A. Khennane, P. J. Hazell, A. M. Remennikov, “Performance of a hybrid GFRP-concrete beam subject to low-velocity impacts,” Composite Structures, vol. 206, pp. 425–438, 2018.

[16] A. Gliszczynski, T. Kubiak, P. Rozylo, P. Jakubczak, J. Bieniaś, “The response of laminated composite plates and profiles under low-velocity impact load,” Composite Structures, vol. 207, pp. 1–12, 2019.

[17] M. Kuhtz, N. Buschner, T. Henseler, A. Hornig, M. Klaerner, M. Ullmann, et al., “An experimental study on the bending response of multi-layered fibre-metal-laminates,” Journal of Composite Materials, vol. 53, no. 18, pp. 2579–2591, 2019.

[18] M. Kashfi, G. H. Majzoobi, N. Bonora, G. Iannitti, A. Ruggiero, E. Khademi, “A study on fiber metal laminates by using a new damage model for composite layer,” International Journal of Mechanical Sciences, vol. 131–132, pp. 75–80, 2017.

[19] P. Jakubczak, J. Bieniaś, M. Droździel, P. Podolak, A. Harmasz, “The effect of layer thicknesses in hybrid titanium-carbon laminates on low-velocity impact response,” Materials, vol. 13, no. 1, p. 103, 2020.

[20] G. Boay, “A review of low-velocity impact on sandwich structures,” Journal of Sandwich Structures and Materials, vol. 15, no. 3, pp. 250–265, 2015.

[21] X. C. Luo, T. Zhang, Q. S. Wang, “Ply thickness’ effect on composite laminate under low-velocity impact,” Advanced Materials Research, vol. 989, pp. 74–78, 2014.

[22] A. Kurşun, M. Şenel, “Investigation of the effect of low-velocity impact on composite plates with preloading,” Experimental Techniques, vol. 37, no. 3, pp. 41–48, 2013.

[23] A. A. Talabari, M. H. Alaei, H. R. Shalian, “Experimental investigation of tensile properties in a glass/epoxy sample manufactured by vacuum infusion, vacuum bag and hand layup process,” Revue des Composites et des Matériaux Avancés, vol. 29, no. 3, pp. 179–182, 2019.

[24] S. Dariushi, S. Farahmandnia, A. M. Rezadoust, “An experimental investigation on infusion time and strength of fiber metal laminates made by vacuum infusion process,” Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications, vol. 235, no. 10, pp. 1800–1808, 2021.

[25] Z. Wen, M. Li, “Numerical study of low-velocity impact response of a fiber composite honeycomb sandwich structure,” Materials, vol. 16, no. 15, p. 5482, 2023.

[26] Y. Ma, D. Bridges, Y. Yu, J. Han, H. Li, A. Hu, “Joining of carbon fiber reinforced plastic to aluminum alloy by reactive multilayer films and low power semiconductor laser heating,” Applied Sciences, vol. 9, no. 2, p. 319, 2019.

[27] G. S. Dhaliwal, G. M. Newaz, “Modeling low velocity impact response of carbon fiber reinforced aluminum laminates (CARALL),” Journal of Dynamic Behavior of Materials, vol. 2, no. 2, pp. 181–193, 2016.

[28] M. O. W. Richardson, M. J. Wisheart, “Review of low-velocity impact properties of composite materials,” Composites Part A: Applied Science and Manufacturing, vol. 27, no. 12, pp. 1123–1131, 1996.

[29] P. Hoang Nam, D. Widagdo, S. Santosa, I. Setya Putra, “Petalling damage analysis of metallic plate structures under localized impact loading—A review,” International Journal of Impact Engineering, vol. 85, no. 5, pp. 100–115, 2015.

[30] F. Zhang, Y. Lin, J. A. Wu, Z. Zhang, Y. Huang, C. Li, et al., “Comparison of stacking sequence on the low-velocity impact failure mechanisms and energy dissipation characteristics of CFRP/Al hybrid laminates,” Polymer Composites, vol. 43, no. 10, pp. 5544–5562, 2022.

[31] N. K. Romli, M. R. M. Rejab, D. Bachtiar, J. Siregar, M. F. Rani, W. S. W. Harun, et al., “The behavior of aluminium carbon/epoxy fibre metal laminate under quasi-static loading,” in IOP Conference Series: Materials Science and Engineering, vol. 257, p. 012046, 2017.

Downloads

Published

2025-09-30

How to Cite

[1]
M. F. Rani, M. R. M. Rejab, N. Ab. Razak, M. I. Ibrahim, M. Z. Azir, and Z. Zaulkafilai, “Assessing the impact resistance and damage tolerance of Aluminium composite fibre metal laminates under low velocity impact test”, J. Mech. Eng. Sci., vol. 19, no. 3, pp. 10727–10738, Sep. 2025, doi: 10.15282/jmes.19.3.2025.3.0841.

Similar Articles

1-10 of 478

You may also start an advanced similarity search for this article.

Most read articles by the same author(s)