Buckling Analysis of Unidirectional Polymer Matrix 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...
Guardado en:
Autor principal: | |
---|---|
Formato: | article |
Lenguaje: | EN |
Publicado: |
Al-Khwarizmi College of Engineering – University of Baghdad
2017
|
Materias: | |
Acceso en línea: | https://doaj.org/article/62f968767fed4dc6a345cec380c0b848 |
Etiquetas: |
Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!
|
id |
oai:doaj.org-article:62f968767fed4dc6a345cec380c0b848 |
---|---|
record_format |
dspace |
spelling |
oai:doaj.org-article:62f968767fed4dc6a345cec380c0b8482021-12-02T07:32:13ZBuckling Analysis of Unidirectional Polymer Matrix Composite Plates1818-11712312-0789https://doaj.org/article/62f968767fed4dc6a345cec380c0b8482017-12-01T00:00:00Zhttp://alkej.uobaghdad.edu.iq/index.php/alkej/article/view/31https://doaj.org/toc/1818-1171https://doaj.org/toc/2312-0789 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. The results show that the maximum value of the critical load is (629.54 N/m) at (q = 0°) and (Vf = 40 %) for the finite element method, while the minimum value of the critical load is (49 N/m) at (q = 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 ( q = 0°) and (Vf = 40 %). Dr. 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 (2017) |
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 Dr. Jawad Kadhim Uleiwi Buckling Analysis of Unidirectional Polymer Matrix 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.
The results show that the maximum value of the critical load is (629.54 N/m) at (q = 0°) and (Vf = 40 %) for the finite element method, while the minimum value of the critical load is (49 N/m) at (q = 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 ( q = 0°) and (Vf = 40 %).
|
format |
article |
author |
Dr. Jawad Kadhim Uleiwi |
author_facet |
Dr. Jawad Kadhim Uleiwi |
author_sort |
Dr. Jawad Kadhim Uleiwi |
title |
Buckling Analysis of Unidirectional Polymer Matrix Composite Plates |
title_short |
Buckling Analysis of Unidirectional Polymer Matrix Composite Plates |
title_full |
Buckling Analysis of Unidirectional Polymer Matrix Composite Plates |
title_fullStr |
Buckling Analysis of Unidirectional Polymer Matrix Composite Plates |
title_full_unstemmed |
Buckling Analysis of Unidirectional Polymer Matrix Composite Plates |
title_sort |
buckling analysis of unidirectional polymer matrix composite plates |
publisher |
Al-Khwarizmi College of Engineering – University of Baghdad |
publishDate |
2017 |
url |
https://doaj.org/article/62f968767fed4dc6a345cec380c0b848 |
work_keys_str_mv |
AT drjawadkadhimuleiwi bucklinganalysisofunidirectionalpolymermatrixcompositeplates |
_version_ |
1718399339227774976 |