The impact behaviour of carbon fiber-epoxy composite leading edge using finite element method

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The impact behaviour of carbon fiber-epoxy composite leading edge using finite element method

Composite material has been widely used in aircrafts due to its high strength to weight ratio that leads to weight saving of the aircrafts. Equally important, aircraft material should be tough i.e. it should have the ability to absorb high energy and thus resist fracture. The aircraft’s wing design...

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Bibliographic Details
Main Authors:	Omar, Nurihan, Aminanda, Yulfian, Mohamed Ali, Jaafar Syed, A. Rasid, Zainudin, Yahaya, Hafizal
Format:	Article
Language:	English English
Published:	Blue Eyes Intelligence Engineering and Sciences Publication 2019
Subjects:	TK Electrical engineering. Electronics Nuclear engineering
Online Access:	http://irep.iium.edu.my/79862/ http://irep.iium.edu.my/79862/1/79862_The%20Impact%20Behaviour%20of%20Carbon.pdf http://irep.iium.edu.my/79862/2/79862_The%20Impact%20Behaviour%20of%20Carbon_SCOPUS.pdf

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