Characterization of Aluminum-E-Glass Fibre - Epoxy Reinforced Fibre Metal Laminates Composites
Keywords:
Chopped Strand Mat (CSM), Fiber Metal Laminates (FML), Glass Fiber reinforced aluminumAbstract
Fiber Metal Laminates (FMLs) are hybrid materials consisting of layers of thin metal sheets and fibres in sandwich pattern. These are best known and extensively used in the Aerospace applications. Aiming this objective, new lightweight FML has been developed by hand layup technique using thin aluminium and E-glass fibres. Tensile tests had been carried out in accordance to ASTM standards to witness the quality of the specimens. From the experimental work, load v/s. displacement and assessing the strength it is observed that the mechanical properties of woven roving mat with aluminum type FML composite proved to be possessing 11.5% higher than the rest of the specimens characterized.
References
- Suyogkumar W. Balbudhe, and Prof. S. R. Zaveri, Stress Analysis Of Riveted Lap Joint, International Journal of Engineering Research & Technology (IJERT), Vol. 2 Issue 3, pp.1-4, 2013.
- Arumulla. Suresh and Tippa Bhimasankara Rao, Analysis of Rivets Using Finite Element Analysis, International Journal of Computational Engineering Research, Vol. 03, Issue 4, pp. 24-27, 2013.
- AdVlot, GLARE –History of the Development of a New Aircraft Material, Kluwer Academic Publishers, ASTM Standard D638-03, D256- 06, D790- 07, D579- 98 (05), 2001,
- P. Kaleeswaran, K. M. Kiran Babu, C. Megala, and B. Sharan Kumar, Fabrication of Fibre Metal Laminate (FML) and Evaluation of Its Mechanical Properties, International Journal of Applied Engineering Research, ISSN 0973-4562 Vol. 9 No.26, pp. 8872-8874, 2014
- Kesavamurthy, Y C et al, Investigation of Tensile Properties of Fibre Reinforced Angle Plate Laminated Composites, International Journal of Emerging Technology and Advanced Engineering, Volume 2, Issue 4, pp.700-703, April 2012.
- Skorupa, M., and Skorupa A., Load transmission and secondary bending in lap joints of aircraft fuselage. Institute of Aviation Scientific Publications, Warsaw, 2010.
- K.Madhan Muthu Ganesh, Damage Tolerant Design for an Aero structural Component, Proceedings of Emerging Trends in Mechanical Engineering, SNS College of Technology, Coimbatore, 2010.
Downloads
Published
Issue
Section
License
Copyright (c) IJSRCSEIT

This work is licensed under a Creative Commons Attribution 4.0 International License.