The Effect of Thicknesses on Impact Damage Advanced Composite Material for Aircraft Application-Reference-Cited by-同舟云学术

The Effect of Thicknesses on Impact Damage Advanced Composite Material for Aircraft Application

Published:2015-04 Issue: Volume:754-755 Page:802-806
ISSN:1662-7482
Container-title:Applied Mechanics and Materials
language:
Short-container-title:AMM

Author:

Syayuthi A.R.¹,Haftirman ¹,Basaruddin K.S.¹,Abdul Manan M.S.¹

Affiliation:

1. Universiti Malaysia Perlis

Abstract

Investigation of impact damage on advanced composite materials of Carbon Fiber Reinforced Epoxy (CFRE) composites and Glass Fiber Reinforced Epoxy (GFRE) composites under high strain rate impact load have been conducted in the present study. Four types of GFRE plates were studied after being impacted with various thicknesses and fixed impact parameters. Results of the present experiments were characterized by the comparison of damage zone among CFRE/GFRE, GFRE with honeycomb core and GFRE without honeycomb core. The result suggests that CFRE is the better structure than GFRE under low velocity impact loads. Higher energy needed to damage the surface of GFRE with core compared to GFRE without core plates.

Publisher

Trans Tech Publications, Ltd.

Link

https://www.scientific.net/AMM.754-755.802.pdf

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