Buckling Analysis of Unidirectional PolymerMatrix Composite Plates

This study deals with the estimation of critical load of unidirectional polymer matrix composite plates by using experimental and finite element techniques at different fiber angles and fiber volume fraction of the composite plate.Buckling analysis illustrated that the critical load decreases in non...

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Autor principal:	Jawad Kadhim Uleiwi
Formato:	article
Lenguaje:	EN
Publicado:	Al-Khwarizmi College of Engineering – University of Baghdad 2006
Materias:	Chemical engineering TP155-156 Engineering (General). Civil engineering (General) TA1-2040
Acceso en línea:	https://doaj.org/article/56c193026f5d41e8a07c3c7424170bb4
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spelling	oai:doaj.org-article:56c193026f5d41e8a07c3c7424170bb42021-12-02T02:42:17ZBuckling Analysis of Unidirectional PolymerMatrix Composite Plates1818-1171https://doaj.org/article/56c193026f5d41e8a07c3c7424170bb42006-01-01T00:00:00Zhttp://www.iasj.net/iasj?func=fulltext&aId=2345https://doaj.org/toc/1818-1171This study deals with the estimation of critical load of unidirectional polymer matrix composite plates by using experimental and finite element techniques at different fiber angles and fiber volume fraction of the composite plate.Buckling analysis illustrated that the critical load decreases in nonlinear relationship with the increase of the fiber angle and that it increases with the increase of the fiber volume fraction.<br />The results show that the maximum value of the critical load is (629.54 N/m) at (? = 0?) and (Vf = 40 %) for the finite element method, while the minimum value of the critical load is (49 N/m) at (? = 90?) and (Vf = 10 %) for the experimental results. The results also indicated that the maximum difference between the finite element analysis and experimental work is about (11 % ) at ( ? = 0?) and (Vf = 40 %)Jawad Kadhim UleiwiAl-Khwarizmi College of Engineering – University of BaghdadarticleChemical engineeringTP155-156Engineering (General). Civil engineering (General)TA1-2040ENAl-Khawarizmi Engineering Journal, Vol 2, Iss 2, Pp 32-45 (2006)
institution	DOAJ
collection	DOAJ
language	EN
topic	Chemical engineering TP155-156 Engineering (General). Civil engineering (General) TA1-2040
spellingShingle	Chemical engineering TP155-156 Engineering (General). Civil engineering (General) TA1-2040 Jawad Kadhim Uleiwi Buckling Analysis of Unidirectional PolymerMatrix Composite Plates
description	This study deals with the estimation of critical load of unidirectional polymer matrix composite plates by using experimental and finite element techniques at different fiber angles and fiber volume fraction of the composite plate.Buckling analysis illustrated that the critical load decreases in nonlinear relationship with the increase of the fiber angle and that it increases with the increase of the fiber volume fraction.<br />The results show that the maximum value of the critical load is (629.54 N/m) at (? = 0?) and (Vf = 40 %) for the finite element method, while the minimum value of the critical load is (49 N/m) at (? = 90?) and (Vf = 10 %) for the experimental results. The results also indicated that the maximum difference between the finite element analysis and experimental work is about (11 % ) at ( ? = 0?) and (Vf = 40 %)
format	article
author	Jawad Kadhim Uleiwi
author_facet	Jawad Kadhim Uleiwi
author_sort	Jawad Kadhim Uleiwi
title	Buckling Analysis of Unidirectional PolymerMatrix Composite Plates
title_short	Buckling Analysis of Unidirectional PolymerMatrix Composite Plates
title_full	Buckling Analysis of Unidirectional PolymerMatrix Composite Plates
title_fullStr	Buckling Analysis of Unidirectional PolymerMatrix Composite Plates
title_full_unstemmed	Buckling Analysis of Unidirectional PolymerMatrix Composite Plates
title_sort	buckling analysis of unidirectional polymermatrix composite plates
publisher	Al-Khwarizmi College of Engineering – University of Baghdad
publishDate	2006
url	https://doaj.org/article/56c193026f5d41e8a07c3c7424170bb4
work_keys_str_mv	AT jawadkadhimuleiwi bucklinganalysisofunidirectionalpolymermatrixcompositeplates
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Buckling Analysis of Unidirectional PolymerMatrix Composite Plates

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