Educational software for stress analysis of an aircraft fuselage

Abstract—A stress analysis software based on MATLAB graphical user interface (GUI) has been developed. The developed software can be used to estimate internal loads on a fuselage and to compute the stresses at any point along the length of the fuselage of a given aircraft. The generalized formulatio...

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Main Authors:	Mohamed Ali, Jaafar Syed, Mustafa Kamal, Izyan Liyana, Ismail, Nurhuda
Format:	Conference or Workshop Item
Language:	English
Published:	2010
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/6586/ http://irep.iium.edu.my/6586/1/papfin.pdf

id	iium-6586
recordtype	eprints
spelling	iium-65862011-11-21T17:55:09Z http://irep.iium.edu.my/6586/ Educational software for stress analysis of an aircraft fuselage Mohamed Ali, Jaafar Syed Mustafa Kamal, Izyan Liyana Ismail, Nurhuda TL500 Aeronautics Abstract—A stress analysis software based on MATLAB graphical user interface (GUI) has been developed. The developed software can be used to estimate internal loads on a fuselage and to compute the stresses at any point along the length of the fuselage of a given aircraft. The generalized formulation allows user to perform stress analysis even on tapered fuselages. The software is expected to be a useful tool for effective teaching learning process of courses on aircraft structures and aircraft structural design. 2010 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/6586/1/papfin.pdf Mohamed Ali, Jaafar Syed and Mustafa Kamal, Izyan Liyana and Ismail, Nurhuda (2010) Educational software for stress analysis of an aircraft fuselage. In: International Conference on Mechanical and Aerospace Engineering (ICMAE 2010), 26-28 Nov 2010, Kuala Lumpur, Malaysia.
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	TL500 Aeronautics
spellingShingle	TL500 Aeronautics Mohamed Ali, Jaafar Syed Mustafa Kamal, Izyan Liyana Ismail, Nurhuda Educational software for stress analysis of an aircraft fuselage
description	Abstract—A stress analysis software based on MATLAB graphical user interface (GUI) has been developed. The developed software can be used to estimate internal loads on a fuselage and to compute the stresses at any point along the length of the fuselage of a given aircraft. The generalized formulation allows user to perform stress analysis even on tapered fuselages. The software is expected to be a useful tool for effective teaching learning process of courses on aircraft structures and aircraft structural design.
format	Conference or Workshop Item
author	Mohamed Ali, Jaafar Syed Mustafa Kamal, Izyan Liyana Ismail, Nurhuda
author_facet	Mohamed Ali, Jaafar Syed Mustafa Kamal, Izyan Liyana Ismail, Nurhuda
author_sort	Mohamed Ali, Jaafar Syed
title	Educational software for stress analysis of an aircraft fuselage
title_short	Educational software for stress analysis of an aircraft fuselage
title_full	Educational software for stress analysis of an aircraft fuselage
title_fullStr	Educational software for stress analysis of an aircraft fuselage
title_full_unstemmed	Educational software for stress analysis of an aircraft fuselage
title_sort	educational software for stress analysis of an aircraft fuselage
publishDate	2010
url	http://irep.iium.edu.my/6586/ http://irep.iium.edu.my/6586/1/papfin.pdf
first_indexed	2023-09-18T20:15:37Z
last_indexed	2023-09-18T20:15:37Z
_version_	1777407767680647168

Educational software for stress analysis of an aircraft fuselage

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