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...

Full description

Bibliographic Details
Main Authors:	Wirawan, Nanda, Abdullah, Nur Azam, Akbar, Mahesa, Curiel-Sosa, J.L.
Format:	Article
Language:	English English
Published:	IOP Publishing Ltd 2018
Subjects:	TL500 Aeronautics
Online Access:	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

id	iium-72822
recordtype	eprints
spelling	iium-728222019-08-19T04:03:53Z 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 Article 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 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. Journal of Physics: Conference Series, 1106. pp. 1-7. ISSN 1742-6588 E-ISSN 1742-6596 https://iopscience.iop.org/article/10.1088/1742-6596/1106/1/012014/pdf 10.1088/1742-6596/1106/1/012014
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English English
topic	TL500 Aeronautics
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
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.
format	Article
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
title	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_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_sort	analysis on cracked commuter aircraft wing under dynamic cruise load by means of xfem
publisher	IOP Publishing Ltd
publishDate	2018
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
first_indexed	2023-09-18T21:43:14Z
last_indexed	2023-09-18T21:43:14Z
_version_	1777413279885295616

Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM

Similar Items