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

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

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...

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Bibliographic Details
Main Authors: Nur Khaleeda, Romli, M. R. M., Rejab, Bachtiar, Dandi, Siregar, J. P., M. F., Rani, W. S., Wan Harun, Salwani, Mohd Salleh, Mohamad Nazirul Mubin, Merzuki
Format: Conference or Workshop Item
Language:English
Published: IOP Publishing 2017
Subjects:
TJ Mechanical engineering and machinery
Online Access:http://umpir.ump.edu.my/id/eprint/19169/
http://umpir.ump.edu.my/id/eprint/19169/
http://umpir.ump.edu.my/id/eprint/19169/
http://umpir.ump.edu.my/id/eprint/19169/1/The%20Behavior%20Of%20Aluminium%20Carbon-Epoxy%20Fibre%20Metal%20Laminate%20Under%20Quasi-Static%20Loading.pdf

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http://umpir.ump.edu.my/id/eprint/19169/
http://umpir.ump.edu.my/id/eprint/19169/
http://umpir.ump.edu.my/id/eprint/19169/
http://umpir.ump.edu.my/id/eprint/19169/1/The%20Behavior%20Of%20Aluminium%20Carbon-Epoxy%20Fibre%20Metal%20Laminate%20Under%20Quasi-Static%20Loading.pdf

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