Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure
The present paper illustrates a modelling technique of void damage prediction using constitutive Rousselier damage model in wingbox aircraft structure. The high possibility of aluminium wingbox structure to deform during operating become a driving force in this study. The Rousselier model is impl...
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| Format: | Article |
| Language: | English |
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IOP Publishing Ltd
2018
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| Online Access: | http://irep.iium.edu.my/73585/ http://irep.iium.edu.my/73585/ http://irep.iium.edu.my/73585/ http://irep.iium.edu.my/73585/1/Ahmad_2018_J._Phys.__Conf._Ser._1106_012013.pdf |
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eprints |
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iium-735852019-08-19T03:45:00Z http://irep.iium.edu.my/73585/ Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure Ahmad, M.I.M. Curiel-Sosa, J.L. Akbar, M. Abdullah, Nur Azam QC Physics T Technology (General) The present paper illustrates a modelling technique of void damage prediction using constitutive Rousselier damage model in wingbox aircraft structure. The high possibility of aluminium wingbox structure to deform during operating become a driving force in this study. The Rousselier model is implemented by the user-defined material subroutine UMAT in the ABAQUS/ Standard. The wingbox is a part of a commercially-made commuter aircraft prototype, in which steady aerodynamic pressure is applied as the quasi-static, ranging from cruise load factor until the ultimate load factor. This analysis is divided into three assessments: load factor assessment, damage detection and implementation of Rousselier-UMAT-XFEM (RuX) model solution. The results indicate the maximum stress concentration occurs at the bottom-root part of the skin. The void volume fraction and the crack grow as the load factor increases to the ultimate load factor. A comparison with the literature is shown in some details. IOP Publishing Ltd 2018-11 Article PeerReviewed application/pdf en http://irep.iium.edu.my/73585/1/Ahmad_2018_J._Phys.__Conf._Ser._1106_012013.pdf Ahmad, M.I.M. and Curiel-Sosa, J.L. and Akbar, M. and Abdullah, Nur Azam (2018) Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure. Journal of Physics: Conference Series, 1106. pp. 1-12. ISSN 1742-6588 E-ISSN 1742-6596 https://iopscience.iop.org/article/10.1088/1742-6596/1106/1/012013/pdf 10.1088/1742-6596/1106/1/012013 |
| repository_type |
Digital Repository |
| institution_category |
Local University |
| institution |
International Islamic University Malaysia |
| building |
IIUM Repository |
| collection |
Online Access |
| language |
English |
| topic |
QC Physics T Technology (General) |
| spellingShingle |
QC Physics T Technology (General) Ahmad, M.I.M. Curiel-Sosa, J.L. Akbar, M. Abdullah, Nur Azam Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure |
| description |
The present paper illustrates a modelling technique of void damage prediction
using constitutive Rousselier damage model in wingbox aircraft structure. The high possibility
of aluminium wingbox structure to deform during operating become a driving force in this
study. The Rousselier model is implemented by the user-defined material subroutine UMAT
in the ABAQUS/ Standard. The wingbox is a part of a commercially-made commuter aircraft
prototype, in which steady aerodynamic pressure is applied as the quasi-static, ranging from
cruise load factor until the ultimate load factor. This analysis is divided into three assessments:
load factor assessment, damage detection and implementation of Rousselier-UMAT-XFEM
(RuX) model solution. The results indicate the maximum stress concentration occurs at the
bottom-root part of the skin. The void volume fraction and the crack grow as the load factor
increases to the ultimate load factor. A comparison with the literature is shown in some details. |
| format |
Article |
| author |
Ahmad, M.I.M. Curiel-Sosa, J.L. Akbar, M. Abdullah, Nur Azam |
| author_facet |
Ahmad, M.I.M. Curiel-Sosa, J.L. Akbar, M. Abdullah, Nur Azam |
| author_sort |
Ahmad, M.I.M. |
| title |
Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure |
| title_short |
Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure |
| title_full |
Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure |
| title_fullStr |
Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure |
| title_full_unstemmed |
Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure |
| title_sort |
numerical inspection based on quasi-static analysis using rousselier damage model for aluminium wingbox aircraft structure |
| publisher |
IOP Publishing Ltd |
| publishDate |
2018 |
| url |
http://irep.iium.edu.my/73585/ http://irep.iium.edu.my/73585/ http://irep.iium.edu.my/73585/ http://irep.iium.edu.my/73585/1/Ahmad_2018_J._Phys.__Conf._Ser._1106_012013.pdf |
| first_indexed |
2023-09-18T21:44:19Z |
| last_indexed |
2023-09-18T21:44:19Z |
| _version_ |
1777413348060561408 |