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Numerical analysis of shot peening parameters for fatigue life improvement

This study will focus on finding the best parameters for shot peening process on aluminium alloy 2024-T351. The main parameters of shot peening process is shot material, velocity, number of impact and also the angle. Strain and work hardening is allowed on the target material. The simulation method...

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Main Authors: Isa M.R., Zaroog O.S., Raj P., Sulaiman S.N., Shah I.A., Ismail I.N., Zahari N.M., Roslan M.E., Mohamed H.
Other Authors: 57193957146
Format: Conference Paper
Published: American Institute of Physics Inc. 2023
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spelling my.uniten.dspace-235772023-05-29T14:50:18Z Numerical analysis of shot peening parameters for fatigue life improvement Isa M.R. Zaroog O.S. Raj P. Sulaiman S.N. Shah I.A. Ismail I.N. Zahari N.M. Roslan M.E. Mohamed H. 57193957146 57189246634 57530239400 57204634551 56737181900 55598767200 54891672300 57189299886 57136356100 This study will focus on finding the best parameters for shot peening process on aluminium alloy 2024-T351. The main parameters of shot peening process is shot material, velocity, number of impact and also the angle. Strain and work hardening is allowed on the target material. The simulation method was performed using ABAQUS 6.11. Simulation was run by applying shots on the aluminum alloy with variable velocity, number of impact as well as the angle of impact. Result shows that by increasing the velocity and the number of impact, the compressive residual stress will significantly increase. The result from the angle simulation shows that the highest impact is caused by an angle of 90�. � 2018 Author(s). Final 2023-05-29T06:50:18Z 2023-05-29T06:50:18Z 2018 Conference Paper 10.1063/1.5066858 2-s2.0-85058011632 https://www.scopus.com/inward/record.uri?eid=2-s2.0-85058011632&doi=10.1063%2f1.5066858&partnerID=40&md5=5a0cfe74f94a1cd663a1c146726b8105 https://irepository.uniten.edu.my/handle/123456789/23577 2030 20217 American Institute of Physics Inc. Scopus
institution Universiti Tenaga Nasional
building UNITEN Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Tenaga Nasional
content_source UNITEN Institutional Repository
url_provider http://dspace.uniten.edu.my/
description This study will focus on finding the best parameters for shot peening process on aluminium alloy 2024-T351. The main parameters of shot peening process is shot material, velocity, number of impact and also the angle. Strain and work hardening is allowed on the target material. The simulation method was performed using ABAQUS 6.11. Simulation was run by applying shots on the aluminum alloy with variable velocity, number of impact as well as the angle of impact. Result shows that by increasing the velocity and the number of impact, the compressive residual stress will significantly increase. The result from the angle simulation shows that the highest impact is caused by an angle of 90�. � 2018 Author(s).
author2 57193957146
author_facet 57193957146
Isa M.R.
Zaroog O.S.
Raj P.
Sulaiman S.N.
Shah I.A.
Ismail I.N.
Zahari N.M.
Roslan M.E.
Mohamed H.
format Conference Paper
author Isa M.R.
Zaroog O.S.
Raj P.
Sulaiman S.N.
Shah I.A.
Ismail I.N.
Zahari N.M.
Roslan M.E.
Mohamed H.
spellingShingle Isa M.R.
Zaroog O.S.
Raj P.
Sulaiman S.N.
Shah I.A.
Ismail I.N.
Zahari N.M.
Roslan M.E.
Mohamed H.
Numerical analysis of shot peening parameters for fatigue life improvement
author_sort Isa M.R.
title Numerical analysis of shot peening parameters for fatigue life improvement
title_short Numerical analysis of shot peening parameters for fatigue life improvement
title_full Numerical analysis of shot peening parameters for fatigue life improvement
title_fullStr Numerical analysis of shot peening parameters for fatigue life improvement
title_full_unstemmed Numerical analysis of shot peening parameters for fatigue life improvement
title_sort numerical analysis of shot peening parameters for fatigue life improvement
publisher American Institute of Physics Inc.
publishDate 2023
_version_ 1806428052971847680
score 13.222552

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