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...
| Main Authors: | , , |
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| Format: | Proceeding Paper |
| Language: | English |
| Published: |
2010
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/6586/ http://irep.iium.edu.my/6586/1/papfin.pdf |
| _version_ | 1848776694726393856 |
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| 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 |
| building | IIUM Repository |
| collection | Online Access |
| 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. |
| first_indexed | 2025-11-14T14:34:10Z |
| format | Proceeding Paper |
| id | iium-6586 |
| institution | International Islamic University Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-14T14:34:10Z |
| publishDate | 2010 |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | iium-65862021-11-11T02:59:34Z 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 Proceeding Paper 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. |
| spellingShingle | TL500 Aeronautics Mohamed Ali, Jaafar Syed Mustafa Kamal, Izyan Liyana Ismail, Nurhuda Educational software for stress analysis of an aircraft fuselage |
| title | 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_short | Educational software for stress analysis of an aircraft fuselage |
| title_sort | educational software for stress analysis of an aircraft fuselage |
| topic | TL500 Aeronautics |
| url | http://irep.iium.edu.my/6586/ http://irep.iium.edu.my/6586/1/papfin.pdf |