Experimental Study of Impact on Carbon-Fiber-Epoxy Composite Wing Leading Edge Structure

Nurihan Omar; Yulfian Aminanda; Jaffar S. Mohamed Ali

doi:10.4028/www.scientific.net/AMM.493.672

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 493Experimental Study of Impact on Carbon-Fiber-Epoxy...

Experimental Study of Impact on Carbon-Fiber-Epoxy Composite Wing Leading Edge Structure

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.

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Periodical:

Applied Mechanics and Materials (Volume 493)

Pages:

672-677

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.493.672

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Online since:

January 2014

Authors:

Nurihan Omar, Yulfian Aminanda, Jaffar S. Mohamed Ali

Keywords:

Composite, Energy Absorption, Impact Loading, Wing Leading Edge

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