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Educational software for stress analysis of an aircraft fuselage

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.

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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.

Item Type: Conference or Workshop Item (Slide Presentation)
Additional Information: 4628/6586
Uncontrolled Keywords: educational software; stress analysis; aircraft fuselage; MATLAB
Subjects: T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL500 Aeronautics
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button): Kulliyyah of Engineering > Department of Mechanical Engineering
Depositing User: Dr Mohamed Ali Jaffar Syed
Date Deposited: 19 Nov 2011 21:37
Last Modified: 11 Nov 2021 10:59
URI: http://irep.iium.edu.my/id/eprint/6586

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