Modelling of transversal crack and delamination under traction with XFEM
This paper presents a new investigation on the computational modelling of crack and delamination on laminates composite. Extended Finite Element Model (XFEM) is used to model the transversal cracks (intralaminar) and delamination (interlaminar). The integration of fracture laws and constitutive equa...
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iium-749712019-10-31T08:27:15Z http://irep.iium.edu.my/74971/ Modelling of transversal crack and delamination under traction with XFEM Abdullah, Nur Azam Curiel-Sosa, J.L. Taylor, Zeike A. Tafazzolimoghaddam, Behrooz Vicente, J.L Martinez TL500 Aeronautics TL787 Astronautics This paper presents a new investigation on the computational modelling of crack and delamination on laminates composite. Extended Finite Element Model (XFEM) is used to model the transversal cracks (intralaminar) and delamination (interlaminar). The integration of fracture laws and constitutive equations are applied to assist the initiation of crack and delamination, and their subsequent evolution. Size effect study for the increment of composite volume on blocking ply is also included in this investigation. The results show very good agreement with the previous experimental and analytical data of each specimen and comparable with the previous literatures by Hallet et al. (transversal crack and delamination) and by Wisnom et al. (laminates size effect study). 2017 Conference or Workshop Item NonPeerReviewed application/pdf en http://irep.iium.edu.my/74971/1/mechcomp-1st%20cert.pdf application/pdf en http://irep.iium.edu.my/74971/7/74971%20Modelling%20of%20transversal%20crack.pdf Abdullah, Nur Azam and Curiel-Sosa, J.L. and Taylor, Zeike A. and Tafazzolimoghaddam, Behrooz and Vicente, J.L Martinez (2017) Modelling of transversal crack and delamination under traction with XFEM. In: 3rd International Conference on Mechanics of Composites (MechComp 2017), 4th-7th July 2017, Bologna, Italy. (Unpublished) |
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TL500 Aeronautics TL787 Astronautics Abdullah, Nur Azam Curiel-Sosa, J.L. Taylor, Zeike A. Tafazzolimoghaddam, Behrooz Vicente, J.L Martinez Modelling of transversal crack and delamination under traction with XFEM |
description |
This paper presents a new investigation on the computational modelling of crack and delamination on laminates composite. Extended Finite Element Model (XFEM) is used to model the transversal cracks (intralaminar) and delamination (interlaminar). The integration of fracture laws and constitutive equations are applied to assist the initiation of crack and delamination, and their subsequent evolution. Size effect study for the increment of composite volume on blocking ply is also included in this investigation. The results show very good agreement with the previous experimental and analytical data of each specimen and comparable with the previous literatures by Hallet et al. (transversal crack and delamination) and by Wisnom et al. (laminates size effect study). |
format |
Conference or Workshop Item |
author |
Abdullah, Nur Azam Curiel-Sosa, J.L. Taylor, Zeike A. Tafazzolimoghaddam, Behrooz Vicente, J.L Martinez |
author_facet |
Abdullah, Nur Azam Curiel-Sosa, J.L. Taylor, Zeike A. Tafazzolimoghaddam, Behrooz Vicente, J.L Martinez |
author_sort |
Abdullah, Nur Azam |
title |
Modelling of transversal crack and delamination under traction with XFEM |
title_short |
Modelling of transversal crack and delamination under traction with XFEM |
title_full |
Modelling of transversal crack and delamination under traction with XFEM |
title_fullStr |
Modelling of transversal crack and delamination under traction with XFEM |
title_full_unstemmed |
Modelling of transversal crack and delamination under traction with XFEM |
title_sort |
modelling of transversal crack and delamination under traction with xfem |
publishDate |
2017 |
url |
http://irep.iium.edu.my/74971/ http://irep.iium.edu.my/74971/1/mechcomp-1st%20cert.pdf http://irep.iium.edu.my/74971/7/74971%20Modelling%20of%20transversal%20crack.pdf |
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2023-09-18T21:46:06Z |
last_indexed |
2023-09-18T21:46:06Z |
_version_ |
1777413460356759552 |