Impact study on aircraft type laminate composite plate: experimental, failure criteria and element model review

This paper reviews the advancement of study of composite laminate subjected to impact loading for aerospace application such as Glass fiber-epoxy and Carbon fiber-epoxy unidirectional laminate plate. The impact testing set-up and equipments are overviewed in this paper including the calculation to o...

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Main Author:	Aminanda, Yulfian
Format:	Book Chapter
Language:	English
Published:	Springer - Verlag 2012
Subjects:	TJ Mechanical engineering and machinery
Online Access:	http://irep.iium.edu.my/23669/ http://irep.iium.edu.my/23669/ http://irep.iium.edu.my/23669/ http://irep.iium.edu.my/23669/1/270012_1_En_11_Chapter_OnlinePDF%5B1%5D_final_version.pdf

id	iium-23669
recordtype	eprints
spelling	iium-236692015-08-26T00:28:07Z http://irep.iium.edu.my/23669/ Impact study on aircraft type laminate composite plate: experimental, failure criteria and element model review Aminanda, Yulfian TJ Mechanical engineering and machinery This paper reviews the advancement of study of composite laminate subjected to impact loading for aerospace application such as Glass fiber-epoxy and Carbon fiber-epoxy unidirectional laminate plate. The impact testing set-up and equipments are overviewed in this paper including the calculation to obtain the force, velocity and energy absorbed by the laminate during impact. The initial damage can be explained by the threshold of energy absorption while the successive damage mechanism can be described by the drop of force obtained from the history of force during impact. The corresponding evidence of damage related to force drop shows the scenario of damage mechanism; matrix cracking, delamination and fiber failure. The influence of projectile and laminate parameters to the impact behavior is reviewed as well. The failure criteria for each phase of damage mechanism are described in detail. The proposed elements model to simulate the damage are overviewed as well, which can be divided into two categories; element without interface layer and with interface layer integrating degradation of mechanical properties. The exposed failure criteria and elements model are the basis of today’s development of FEA simulation for impact purpose. Springer - Verlag 2012-01-04 Book Chapter PeerReviewed application/pdf en http://irep.iium.edu.my/23669/1/270012_1_En_11_Chapter_OnlinePDF%5B1%5D_final_version.pdf Aminanda, Yulfian (2012) Impact study on aircraft type laminate composite plate: experimental, failure criteria and element model review. In: Damage and fracture of composite sand structure. Advanced structure materials, 17 (17). Springer - Verlag, Berlin Germany, pp. 157-186. ISBN 9783642236587 http://rd.springer.com/chapter/10.1007/978-3-642-23659-4_11# 10.1007/978-3-642-23659-4_11
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	TJ Mechanical engineering and machinery
spellingShingle	TJ Mechanical engineering and machinery Aminanda, Yulfian Impact study on aircraft type laminate composite plate: experimental, failure criteria and element model review
description	This paper reviews the advancement of study of composite laminate subjected to impact loading for aerospace application such as Glass fiber-epoxy and Carbon fiber-epoxy unidirectional laminate plate. The impact testing set-up and equipments are overviewed in this paper including the calculation to obtain the force, velocity and energy absorbed by the laminate during impact. The initial damage can be explained by the threshold of energy absorption while the successive damage mechanism can be described by the drop of force obtained from the history of force during impact. The corresponding evidence of damage related to force drop shows the scenario of damage mechanism; matrix cracking, delamination and fiber failure. The influence of projectile and laminate parameters to the impact behavior is reviewed as well. The failure criteria for each phase of damage mechanism are described in detail. The proposed elements model to simulate the damage are overviewed as well, which can be divided into two categories; element without interface layer and with interface layer integrating degradation of mechanical properties. The exposed failure criteria and elements model are the basis of today’s development of FEA simulation for impact purpose.
format	Book Chapter
author	Aminanda, Yulfian
author_facet	Aminanda, Yulfian
author_sort	Aminanda, Yulfian
title	Impact study on aircraft type laminate composite plate: experimental, failure criteria and element model review
title_short	Impact study on aircraft type laminate composite plate: experimental, failure criteria and element model review
title_full	Impact study on aircraft type laminate composite plate: experimental, failure criteria and element model review
title_fullStr	Impact study on aircraft type laminate composite plate: experimental, failure criteria and element model review
title_full_unstemmed	Impact study on aircraft type laminate composite plate: experimental, failure criteria and element model review
title_sort	impact study on aircraft type laminate composite plate: experimental, failure criteria and element model review
publisher	Springer - Verlag
publishDate	2012
url	http://irep.iium.edu.my/23669/ http://irep.iium.edu.my/23669/ http://irep.iium.edu.my/23669/ http://irep.iium.edu.my/23669/1/270012_1_En_11_Chapter_OnlinePDF%5B1%5D_final_version.pdf
first_indexed	2023-09-18T20:35:46Z
last_indexed	2023-09-18T20:35:46Z
_version_	1777409035374428160

Impact study on aircraft type laminate composite plate: experimental, failure criteria and element model review

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