Improvement of Mechanical and Fatigue Properties for Aluminum Alloy 7049 By Using Nano Composites Technique

The aim of present work is to improve mechanical and fatigue properties for Aluminum alloy7049 by using Nano composites technique. The ZrO2 with an average grain diameter of 30-40 nm, was selected as Nano particles, to reinforce Aluminum alloy7049 with different percentage as, 2, 4, 6 and 7 %. The...

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Autores principales: Alalkawi H. J. M., Ali Yousuf K Khenyab, Abduljabar H. Ali
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Lenguaje:EN
Publicado: Al-Khwarizmi College of Engineering – University of Baghdad 2019
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Acceso en línea:https://doaj.org/article/6c33d6fb13634283a29101cc18738002
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spelling oai:doaj.org-article:6c33d6fb13634283a29101cc187380022021-12-02T05:46:59ZImprovement of Mechanical and Fatigue Properties for Aluminum Alloy 7049 By Using Nano Composites Technique10.22153/kej.2019.08.0011818-11712312-0789https://doaj.org/article/6c33d6fb13634283a29101cc187380022019-03-01T00:00:00Zhttp://alkej.uobaghdad.edu.iq/index.php/alkej/article/view/410https://doaj.org/toc/1818-1171https://doaj.org/toc/2312-0789 The aim of present work is to improve mechanical and fatigue properties for Aluminum alloy7049 by using Nano composites technique. The ZrO2 with an average grain diameter of 30-40 nm, was selected as Nano particles, to reinforce Aluminum alloy7049 with different percentage as, 2, 4, 6 and 7 %. The Stir casting method was used to fabricate the Nano composites materials due to economical route for improvement and processing of metal matrix composites. The experimental results were shown that the adding of zirconium oxide (ZrO2) as reinforced material leads to improve mechanical properties. The best percentage of improvement of mechanical properties of 7049 AA was with 4% wt. of ZrO2 about (7.76% ) for ultimate tensile stress UTS, (9.62% ) for yield stress YS and (9.92%) for hardness HB than other of adding of 2, 6 and 7% of ZrO2. Also the results shown that the fatigue strength of 7049 AA with 4 % ZrO2 nanoparticles is higher than that of 7049 AA under constant loading 9.86% at 108 cycles as well as the fatigue life factor (IFLF %) at different amplitude stress 400, 350, 300 and 250 MPa  was improvement in range 66, 115, 63 and 107%  respectively. Alalkawi H. J. M.Ali Yousuf K KhenyabAbduljabar H. AliAl-Khwarizmi College of Engineering – University of BaghdadarticleNanomaterial, 7049 AA, ZrO2, Stir casting.Chemical engineeringTP155-156Engineering (General). Civil engineering (General)TA1-2040ENAl-Khawarizmi Engineering Journal, Vol 15, Iss 1 (2019)
institution DOAJ
collection DOAJ
language EN
topic Nanomaterial, 7049 AA, ZrO2, Stir casting.
Chemical engineering
TP155-156
Engineering (General). Civil engineering (General)
TA1-2040
spellingShingle Nanomaterial, 7049 AA, ZrO2, Stir casting.
Chemical engineering
TP155-156
Engineering (General). Civil engineering (General)
TA1-2040
Alalkawi H. J. M.
Ali Yousuf K Khenyab
Abduljabar H. Ali
Improvement of Mechanical and Fatigue Properties for Aluminum Alloy 7049 By Using Nano Composites Technique
description The aim of present work is to improve mechanical and fatigue properties for Aluminum alloy7049 by using Nano composites technique. The ZrO2 with an average grain diameter of 30-40 nm, was selected as Nano particles, to reinforce Aluminum alloy7049 with different percentage as, 2, 4, 6 and 7 %. The Stir casting method was used to fabricate the Nano composites materials due to economical route for improvement and processing of metal matrix composites. The experimental results were shown that the adding of zirconium oxide (ZrO2) as reinforced material leads to improve mechanical properties. The best percentage of improvement of mechanical properties of 7049 AA was with 4% wt. of ZrO2 about (7.76% ) for ultimate tensile stress UTS, (9.62% ) for yield stress YS and (9.92%) for hardness HB than other of adding of 2, 6 and 7% of ZrO2. Also the results shown that the fatigue strength of 7049 AA with 4 % ZrO2 nanoparticles is higher than that of 7049 AA under constant loading 9.86% at 108 cycles as well as the fatigue life factor (IFLF %) at different amplitude stress 400, 350, 300 and 250 MPa  was improvement in range 66, 115, 63 and 107%  respectively.
format article
author Alalkawi H. J. M.
Ali Yousuf K Khenyab
Abduljabar H. Ali
author_facet Alalkawi H. J. M.
Ali Yousuf K Khenyab
Abduljabar H. Ali
author_sort Alalkawi H. J. M.
title Improvement of Mechanical and Fatigue Properties for Aluminum Alloy 7049 By Using Nano Composites Technique
title_short Improvement of Mechanical and Fatigue Properties for Aluminum Alloy 7049 By Using Nano Composites Technique
title_full Improvement of Mechanical and Fatigue Properties for Aluminum Alloy 7049 By Using Nano Composites Technique
title_fullStr Improvement of Mechanical and Fatigue Properties for Aluminum Alloy 7049 By Using Nano Composites Technique
title_full_unstemmed Improvement of Mechanical and Fatigue Properties for Aluminum Alloy 7049 By Using Nano Composites Technique
title_sort improvement of mechanical and fatigue properties for aluminum alloy 7049 by using nano composites technique
publisher Al-Khwarizmi College of Engineering – University of Baghdad
publishDate 2019
url https://doaj.org/article/6c33d6fb13634283a29101cc18738002
work_keys_str_mv AT alalkawihjm improvementofmechanicalandfatiguepropertiesforaluminumalloy7049byusingnanocompositestechnique
AT aliyousufkkhenyab improvementofmechanicalandfatiguepropertiesforaluminumalloy7049byusingnanocompositestechnique
AT abduljabarhali improvementofmechanicalandfatiguepropertiesforaluminumalloy7049byusingnanocompositestechnique
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