UMP Institutional Repository

The Behavior Of Aluminium Carbon/Epoxy Fibre Metal Laminate Under Quasi-Static Loading

Nur Khaleeda, Romli and M. R. M., Rejab and Bachtiar, Dandi and Siregar, J. P. and M. F., Rani and W. S., Wan Harun and Salwani, Mohd Salleh and Mohamad Nazirul Mubin, Merzuki (2017) The Behavior Of Aluminium Carbon/Epoxy Fibre Metal Laminate Under Quasi-Static Loading. In: 4th International Conference on Mechanical Engineering Research (ICMER2017), 1–2 August 2017 , Swiss Garden Beach Resort, Kuantan, Pahang, Malaysia. pp. 1-12., 257 (012046). ISSN 1757-8981 (Print); 1757-899X (Online)

[img]
Preview
PDF
The Behavior Of Aluminium Carbon-Epoxy Fibre Metal Laminate Under Quasi-Static Loading.pdf
Available under License Creative Commons Attribution.

Download (268kB) | Preview

Abstract

One of major concerns that related to the flight safety is impact of birds. To minimize the risks, there is need to increase the impact resistance of aircraft by developing a new material and has the good structural design of aircraft structures. The hybrid laminates are potential candidate material to be applied for the aircraft structures susceptible to bird strikes. The fibre metal laminate was fabricated by a compression moulding technique. The carbon fibre and aluminium alloy 2024-0 was laminated by using thermoset epoxy. A compression moulding technique was used for the FML fabrication. The aluminium sheet metal has been roughening by a metal sanding method which to improve the bonding between the fibre and metal layer. The main objective of this paper is to determine the failure response of the laminate under five variations of the crosshead displacement in the quasi-static loading. The FML was modelled and analysed by using Explicit solver. Based on the experimental data of the quasi-static test, the result of 1 mm/min was 11.85 kN and higher than 5, 10, 50 and 100 mm/min which because of the aluminium ductility during the impact loading response. The numerical simulations were generally in good agreement with the experimental measurements.

Item Type: Conference or Workshop Item (Speech)
Subjects: T Technology > TJ Mechanical engineering and machinery
Faculty/Division: Faculty of Mechanical Engineering
Depositing User: Mrs. Neng Sury Sulaiman
Date Deposited: 27 Nov 2017 03:15
Last Modified: 11 Jan 2018 00:02
URI: http://umpir.ump.edu.my/id/eprint/19169
Download Statistic: View Download Statistics

Actions (login required)

View Item View Item