Development of educational software for stress analysis of an aircraft wing

Mohamed Ali, Jaafar Syed and Sadeq, Tazkera (2012) Development of educational software for stress analysis of an aircraft wing. Journal of Engineering Science and Technology , 7 (3). pp. 322-338. ISSN 1823-4690

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Abstract

A stress analysis software based on MATLAB, Graphic user interface (GUI) has been developed. The developed software can be used to estimate load on a wing and to compute the stresses at any point along the span of the wing of a given aircraft. The generalized formulation allows performing stress analysis even for a multispar (multicell) wing. The software is expected to be a useful tool for effective teaching learning process of courses on aircraft structures and aircraft structural design.

Item Type:	Article (Journal)
Additional Information:	4262/29145
Uncontrolled Keywords:	Education, Software, Stress analysis, Aircraft wings, MATLAB.
Subjects:	T Technology > TA Engineering (General). Civil engineering (General) > TA349 Mechanics of engineering. Applied mechanics
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button):	Kulliyyah of Engineering > Department of Mechanical Engineering
Depositing User:	Nur' Aini Abu Bakar
Date Deposited:	26 Feb 2013 10:39
Last Modified:	26 Feb 2013 10:39
URI:	http://irep.iium.edu.my/id/eprint/29145

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