A matlab based educational software for the study on the effect of cut-out in aircraft wings

Mohammed Riyadh, Miah and Syed Mohamed Ali, Jaffar (2018) A matlab based educational software for the study on the effect of cut-out in aircraft wings. International Journal of Engineering & Technology, 7 (4.25). pp. 114-118. ISSN 2227-524X

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Abstract

Cut-outs on aircraft wings are unavoidable due to the placement of fuel tanks and retraction of landing gear inside the wing. The stresses acting on an aircraft wing will deviate substantially before and after a cut-out is made and therefore it is crucial to perform stress analysis in an aircraft wing in order to ensure that the wing structure will be able to withstand the applied stress. Stress analysis of such structures is tedious and time consuming due to its statically indeterminate nature. A free stand-alone software based on MATLAB for the computation of stress due to the effect of cut-out in idealized wing torsion box has been developed. The main purpose is to provide the end-user (student or academic) a useful and user-friendly tool to perform preliminary stress assessment of the effect of cut-out analysis for an idealized wing.

Item Type:	Article (Journal)
Additional Information:	4262/68441
Uncontrolled Keywords:	Stress Analysis, Cut-out, Wing, MATLAB, Aircraft Structures
Subjects:	T Technology > TL Motor vehicles. Aeronautics. Astronautics 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 Kulliyyah of Engineering > Department of Mechanical Engineering
Depositing User:	Dr Mohamed Ali Jaffar Syed
Date Deposited:	18 Dec 2018 14:21
Last Modified:	18 Dec 2018 14:21
URI:	http://irep.iium.edu.my/id/eprint/68441

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