Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM
In this paper, a new investigation of crack propagation on a commuter aircraft wing is discussed. The aircraft is a 19-seater multi-purpose commuter aircraft designed for a mission on the remote area. The dynamic load acting on the wing is assumed as harmonic load considering aerodynamic lift at...
| Main Authors: | , , , |
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| Format: | Proceeding Paper |
| Language: | English English English |
| Published: |
IOP Publishing Ltd
2018
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/72822/ http://irep.iium.edu.my/72822/1/72822%20Analysis%20on%20Cracked%20Commuter.pdf http://irep.iium.edu.my/72822/2/72822%20Analysis%20on%20Cracked%20Commuter%20SCOPUS.pdf http://irep.iium.edu.my/72822/13/72822%20slides.pdf |
| _version_ | 1848787687079673856 |
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| author | Wirawan, Nanda Abdullah, Nur Azam Akbar, Mahesa Curiel-Sosa, J.L. |
| author_facet | Wirawan, Nanda Abdullah, Nur Azam Akbar, Mahesa Curiel-Sosa, J.L. |
| author_sort | Wirawan, Nanda |
| building | IIUM Repository |
| collection | Online Access |
| description | In this paper, a new investigation of crack propagation on a commuter aircraft
wing is discussed. The aircraft is a 19-seater multi-purpose commuter aircraft designed for a
mission on the remote area. The dynamic load acting on the wing is assumed as harmonic
load considering aerodynamic lift at a particular excitation frequency. A 3D wingbox CAD
model is developed for the numerical simulation. Extended finite element (XFEM) is applied to
analyse the crack propagation on the aircraft wing. The crack growth simulation is successfully
done, and the results are shown in some details. These results provided a novel insight on the
computational simulation of cracked wing structure under dynamic flight load. |
| first_indexed | 2025-11-14T17:28:53Z |
| format | Proceeding Paper |
| id | iium-72822 |
| institution | International Islamic University Malaysia |
| institution_category | Local University |
| language | English English English |
| last_indexed | 2025-11-14T17:28:53Z |
| publishDate | 2018 |
| publisher | IOP Publishing Ltd |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | iium-728222020-12-22T02:51:16Z http://irep.iium.edu.my/72822/ Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM Wirawan, Nanda Abdullah, Nur Azam Akbar, Mahesa Curiel-Sosa, J.L. TL500 Aeronautics In this paper, a new investigation of crack propagation on a commuter aircraft wing is discussed. The aircraft is a 19-seater multi-purpose commuter aircraft designed for a mission on the remote area. The dynamic load acting on the wing is assumed as harmonic load considering aerodynamic lift at a particular excitation frequency. A 3D wingbox CAD model is developed for the numerical simulation. Extended finite element (XFEM) is applied to analyse the crack propagation on the aircraft wing. The crack growth simulation is successfully done, and the results are shown in some details. These results provided a novel insight on the computational simulation of cracked wing structure under dynamic flight load. IOP Publishing Ltd 2018-11-05 Proceeding Paper PeerReviewed application/pdf en http://irep.iium.edu.my/72822/1/72822%20Analysis%20on%20Cracked%20Commuter.pdf application/pdf en http://irep.iium.edu.my/72822/2/72822%20Analysis%20on%20Cracked%20Commuter%20SCOPUS.pdf application/pdf en http://irep.iium.edu.my/72822/13/72822%20slides.pdf Wirawan, Nanda and Abdullah, Nur Azam and Akbar, Mahesa and Curiel-Sosa, J.L. (2018) Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM. In: Modern Practice in Stress and Vibration Analysis (MPSVA) 2018, 2nd-4th July 2018, Cambridge, UK. https://iopscience.iop.org/article/10.1088/1742-6596/1106/1/012014/pdf 10.1088/1742-6596/1106/1/012014 |
| spellingShingle | TL500 Aeronautics Wirawan, Nanda Abdullah, Nur Azam Akbar, Mahesa Curiel-Sosa, J.L. Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM |
| title | Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM |
| title_full | Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM |
| title_fullStr | Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM |
| title_full_unstemmed | Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM |
| title_short | Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM |
| title_sort | analysis on cracked commuter aircraft wing under dynamic cruise load by means of xfem |
| topic | TL500 Aeronautics |
| url | http://irep.iium.edu.my/72822/ http://irep.iium.edu.my/72822/ http://irep.iium.edu.my/72822/ http://irep.iium.edu.my/72822/1/72822%20Analysis%20on%20Cracked%20Commuter.pdf http://irep.iium.edu.my/72822/2/72822%20Analysis%20on%20Cracked%20Commuter%20SCOPUS.pdf http://irep.iium.edu.my/72822/13/72822%20slides.pdf |