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

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 cur...

Full description

Bibliographic Details
Main Authors:	Omar, Nurihan, Aminanda, Yulfian, Syed Mohamed Ali, Jaffar
Format:	Article
Language:	English English
Published:	Trans Tech Publications Ltd., Switzerland 2014
Subjects:	TK Electrical engineering. Electronics Nuclear engineering
Online Access:	http://irep.iium.edu.my/34928/ http://irep.iium.edu.my/34928/ http://irep.iium.edu.my/34928/1/experimental_study_of_impact_on_carbon_fiber_epoxy_composite_wiing_leading_edge.pdf http://irep.iium.edu.my/34928/4/34928_Experimental%20study%20of%20impact%20on%20carbon-fiber-epoxy%20composite%20wing%20leading_Scopus.pdf

id	iium-34928
recordtype	eprints
spelling	iium-349282017-09-06T03:53:29Z http://irep.iium.edu.my/34928/ Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure Omar, Nurihan Aminanda, Yulfian Syed Mohamed Ali, Jaffar TK Electrical engineering. Electronics Nuclear engineering 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. Trans Tech Publications Ltd., Switzerland 2014 Article PeerReviewed application/pdf en http://irep.iium.edu.my/34928/1/experimental_study_of_impact_on_carbon_fiber_epoxy_composite_wiing_leading_edge.pdf application/pdf en http://irep.iium.edu.my/34928/4/34928_Experimental%20study%20of%20impact%20on%20carbon-fiber-epoxy%20composite%20wing%20leading_Scopus.pdf 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 doi:10.4028/www.scientific.net/AMM.493.672
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English English
topic	TK Electrical engineering. Electronics Nuclear engineering
spellingShingle	TK Electrical engineering. Electronics Nuclear engineering Omar, Nurihan Aminanda, Yulfian Syed Mohamed Ali, Jaffar Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure
description	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.
format	Article
author	Omar, Nurihan Aminanda, Yulfian Syed Mohamed Ali, Jaffar
author_facet	Omar, Nurihan Aminanda, Yulfian Syed Mohamed Ali, Jaffar
author_sort	Omar, Nurihan
title	Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure
title_short	Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure
title_full	Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure
title_fullStr	Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure
title_full_unstemmed	Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure
title_sort	experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure
publisher	Trans Tech Publications Ltd., Switzerland
publishDate	2014
url	http://irep.iium.edu.my/34928/ http://irep.iium.edu.my/34928/ http://irep.iium.edu.my/34928/1/experimental_study_of_impact_on_carbon_fiber_epoxy_composite_wiing_leading_edge.pdf http://irep.iium.edu.my/34928/4/34928_Experimental%20study%20of%20impact%20on%20carbon-fiber-epoxy%20composite%20wing%20leading_Scopus.pdf
first_indexed	2023-09-18T20:50:13Z
last_indexed	2023-09-18T20:50:13Z
_version_	1777409944345116672

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

Similar Items