Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure

Omar, Nurihan and Aminanda, Yulfian and Syed Mohamed Ali, Jaffar (2014) Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure. Applied Mechanics and Materials, 493. pp. 672-677. ISSN 1660-9336

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Abstract

This paper works on the curvature composite structure for wing leading edge application using fabric carbon/epoxy material subjected to impact loading. At first stage, rigid spherical projectile and elliptical panel with were used. The impact testing has been carried out by varying the radius of curvature, the thickness of the panel and different stacking sequence. The experimental results show the trend of specific energy absorption capability of structure in function of the radius, thickness of panel and carbon fiber directions.

Item Type:	Article (Journal)
Additional Information:	5168/34928
Uncontrolled Keywords:	composite,wing leading edge, impact loading, energy absorption
Subjects:	T Technology > TK Electrical engineering. Electronics Nuclear engineering
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button):	Kulliyyah of Engineering > Department of Mechanical Engineering
Depositing User:	Prof Dr Ing yulfian aminanda
Date Deposited:	06 Feb 2014 11:28
Last Modified:	06 Sep 2017 11:53
URI:	http://irep.iium.edu.my/id/eprint/34928

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