Studying the Tensile and Buckling for PMMA Reinforced by Jute Fibers for Prosthetic Pylon

The main objective of this research is studying the tensile and buckling of Jute fibers reinforced composite by varying the number of Jute fibers layers and fibers angle (±45°&0°/90°). Vacuum bagging technique was adopted for the preparation of laminated composite specimens that made from PMMA a...

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Main Authors: Jawad Kadhim Oleiwi, Shaymaa Jumaah Ahmed
Format: Article
Language:English
Published: Unviversity of Technology- Iraq 2016-01-01
Series:Engineering and Technology Journal
Subjects:
Online Access:https://etj.uotechnology.edu.iq/article_112545_4927b5c897b0b1bc15805a9fa5f3c514.pdf
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author Jawad Kadhim Oleiwi
Shaymaa Jumaah Ahmed
author_facet Jawad Kadhim Oleiwi
Shaymaa Jumaah Ahmed
author_sort Jawad Kadhim Oleiwi
collection DOAJ
description The main objective of this research is studying the tensile and buckling of Jute fibers reinforced composite by varying the number of Jute fibers layers and fibers angle (±45°&0°/90°). Vacuum bagging technique was adopted for the preparation of laminated composite specimens that made from PMMA as matrix and Perlon layers with different number of Jute fibers layers as reinforcement materials. Also the finite element method (ANSYS-15) was used by creating a model of prosthetic pylon and applied compressive load at heel strike step from gait cycle to know the critical buckling stress. The results showed that the best laminated composite specimens have three Jute fibers layers at (0 º /90 º) fibers orientation relative to applied load. Where, the critical buckling stress, tensile strength, and modulus of elasticity were (442MPa, 61MPa, and 3.75GPa) respectively, while, the percentage elongation was (2.1).
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spelling doaj.art-dc31e8cddc2a4a8596a865e3b63833ba2024-02-04T17:27:21ZengUnviversity of Technology- IraqEngineering and Technology Journal1681-69002412-07582016-01-01341A11112210.30684/etj.34.1A.10112545Studying the Tensile and Buckling for PMMA Reinforced by Jute Fibers for Prosthetic PylonJawad Kadhim OleiwiShaymaa Jumaah AhmedThe main objective of this research is studying the tensile and buckling of Jute fibers reinforced composite by varying the number of Jute fibers layers and fibers angle (±45°&0°/90°). Vacuum bagging technique was adopted for the preparation of laminated composite specimens that made from PMMA as matrix and Perlon layers with different number of Jute fibers layers as reinforcement materials. Also the finite element method (ANSYS-15) was used by creating a model of prosthetic pylon and applied compressive load at heel strike step from gait cycle to know the critical buckling stress. The results showed that the best laminated composite specimens have three Jute fibers layers at (0 º /90 º) fibers orientation relative to applied load. Where, the critical buckling stress, tensile strength, and modulus of elasticity were (442MPa, 61MPa, and 3.75GPa) respectively, while, the percentage elongation was (2.1).https://etj.uotechnology.edu.iq/article_112545_4927b5c897b0b1bc15805a9fa5f3c514.pdfprosthetic pylonjute fiberstensilebuckling
spellingShingle Jawad Kadhim Oleiwi
Shaymaa Jumaah Ahmed
Studying the Tensile and Buckling for PMMA Reinforced by Jute Fibers for Prosthetic Pylon
Engineering and Technology Journal
prosthetic pylon
jute fibers
tensile
buckling
title Studying the Tensile and Buckling for PMMA Reinforced by Jute Fibers for Prosthetic Pylon
title_full Studying the Tensile and Buckling for PMMA Reinforced by Jute Fibers for Prosthetic Pylon
title_fullStr Studying the Tensile and Buckling for PMMA Reinforced by Jute Fibers for Prosthetic Pylon
title_full_unstemmed Studying the Tensile and Buckling for PMMA Reinforced by Jute Fibers for Prosthetic Pylon
title_short Studying the Tensile and Buckling for PMMA Reinforced by Jute Fibers for Prosthetic Pylon
title_sort studying the tensile and buckling for pmma reinforced by jute fibers for prosthetic pylon
topic prosthetic pylon
jute fibers
tensile
buckling
url https://etj.uotechnology.edu.iq/article_112545_4927b5c897b0b1bc15805a9fa5f3c514.pdf
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