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

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 wi...

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Main Authors: Mohammed Riyadh, Miah, Syed Mohamed Ali, Jaffar
Format: Article
Language:English
English
Published: Science Publishing Corporation Inc 2018
Subjects:
TL Motor vehicles. Aeronautics. Astronautics
TL500 Aeronautics
Online Access:http://irep.iium.edu.my/68441/1/68441_A%20Matlab%20Based%20Educational%20Software.pdf
http://irep.iium.edu.my/68441/2/68441_A%20Matlab%20Based%20Educational%20Software_SCOPUS.pdf
http://irep.iium.edu.my/68441/
https://www.sciencepubco.com/index.php/ijet/article/view/22409
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spelling my.iium.irep.684412018-12-18T06:21:29Z http://irep.iium.edu.my/68441/ A matlab based educational software for the study on the effect of cut-out in aircraft wings Mohammed Riyadh, Miah Syed Mohamed Ali, Jaffar TL Motor vehicles. Aeronautics. Astronautics TL500 Aeronautics 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. Science Publishing Corporation Inc 2018-11-30 Article PeerReviewed application/pdf en http://irep.iium.edu.my/68441/1/68441_A%20Matlab%20Based%20Educational%20Software.pdf application/pdf en http://irep.iium.edu.my/68441/2/68441_A%20Matlab%20Based%20Educational%20Software_SCOPUS.pdf 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 https://www.sciencepubco.com/index.php/ijet/article/view/22409 10.14419/ijet.v7i4.25.22409
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
English
topic TL Motor vehicles. Aeronautics. Astronautics
TL500 Aeronautics
spellingShingle TL Motor vehicles. Aeronautics. Astronautics
TL500 Aeronautics
Mohammed Riyadh, Miah
Syed Mohamed Ali, Jaffar
A matlab based educational software for the study on the effect of cut-out in aircraft wings
description 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.
format Article
author Mohammed Riyadh, Miah
Syed Mohamed Ali, Jaffar
author_facet Mohammed Riyadh, Miah
Syed Mohamed Ali, Jaffar
author_sort Mohammed Riyadh, Miah
title A matlab based educational software for the study on the effect of cut-out in aircraft wings
title_short A matlab based educational software for the study on the effect of cut-out in aircraft wings
title_full A matlab based educational software for the study on the effect of cut-out in aircraft wings
title_fullStr A matlab based educational software for the study on the effect of cut-out in aircraft wings
title_full_unstemmed A matlab based educational software for the study on the effect of cut-out in aircraft wings
title_sort matlab based educational software for the study on the effect of cut-out in aircraft wings
publisher Science Publishing Corporation Inc
publishDate 2018
url http://irep.iium.edu.my/68441/1/68441_A%20Matlab%20Based%20Educational%20Software.pdf
http://irep.iium.edu.my/68441/2/68441_A%20Matlab%20Based%20Educational%20Software_SCOPUS.pdf
http://irep.iium.edu.my/68441/
https://www.sciencepubco.com/index.php/ijet/article/view/22409
_version_ 1643618602755031040
score 13.211869

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