Impact Test on Laminate Composites of Carbon Steel (SAE 1042) Epoxy and Aluminium Alloy (6061- T6) At Room Temperature
DOI:
https://doi.org/10.24113/ijoscience.v9i7.505Abstract
This research paper focuses on the laminate composites of carbon steel and aluminium alloy using epoxy resin. For making composite metal laminates, compression molding method is used. Press is used for making sandwiched plates at 90°C for 155 seconds. Izod and Charpy Impact test were performed on the laminated composites and its parent material i.e., Carbon Steel (SAE1042) and Aluminium Alloy (6061-T6) to made a comparison with its composites and to investigate the suitability of the material for a specific application and in predicting its expected service life.
Downloads
Metrics
References
Binbin Liao, Jianwu Zhou, Ying Li, Panding Wang, Li Xi, Ruxin Gao, Ke Bo, and Daining Fang, “Damage accumulation mechanism of composite laminates subjected to repeated low velocity impacts”, International Journal of Mechanical Sciences, MS 105783 2020
V. M. Gayatri, T. Gayathri and A. Krishnaiah, “Impact behaviour of Fibre Reinforced composites with change in Fibre Orientation”, International Journal of Current Engineering and Technology (2016) 1-10.
Ajay Kumar Kaviti, Kiran Kumar Namala, G. Srinivasa Gupta, and Ch. Naveen Reddy, “Modeling and Simulation on Composite Laminates Subjected To Low Velocity Impact”, Materials Today: Proceedings 18 (2019) 5364–5372
J.J.C. Remmers, R. de Borst, “Delamination buckling of fibre–metal laminates”, Composites Science and Technology,61(2001) 2207–2213
Metin Sayer, Numan B. Bektas, Ersin Demir, Hasan Calliog, “The effect of temperatures on hybrid composite laminates under impact loading”,Composites Part B: Engineering 43 (2012) 2152–2160
Ruys D, Crosky A, and Evans WJ. “Natural bast fibre structure”, International Journal of Materials and Product Technology 17(2002) 2-10.
Aniello Riccio, Salvatore Saputo, Andrea Sellitto, Angela Russo, Valerio Acanfora, Paola Iaccarino, Mauro Zarrelli.,“Mechanical behaviour of laminated composite plates subjected to compression after impact tests”, Materials Today: Proceedings 34(2021), 53-56
R.V. Choudri, S.C. Soni, A. N. Mathur., “Tensile Fracture strength of Boron (SAE-1042)/Epoxy/Aluminium(6061-t6) laminates”, Materials Today: Proceedings 4 (2017) 3407–3415
Downloads
Published
How to Cite
Issue
Section
License
Copyright (c) 2023 Kamran Karim Khan, Sanjay Chhalotre
This work is licensed under a Creative Commons Attribution 4.0 International License.
IJOSCIENCE follows an Open Journal Access policy. Authors retain the copyright of the original work and grant the rights of publication to the publisher with the work simultaneously licensed under a Creative Commons CC BY License that allows others to distribute, remix, adapt, and build upon your work, even commercially, as long as they credit you for the original creation. Authors are permitted to post their work in institutional repositories, social media or other platforms.
Under the following terms:
-
Attribution — You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use.
- No additional restrictions — You may not apply legal terms or technological measures that legally restrict others from doing anything the license permits.
