Development of educational software for stress analysis of an aircraft wing
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 allow...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Taylor's University
2012
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/29145/ http://irep.iium.edu.my/29145/1/DEVELOPMENT_OF_EDUCATIONAL_SOFTWARE.pdf |
| _version_ | 1848780070178521088 |
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| author | Mohamed Ali, Jaafar Syed Sadeq, Tazkera |
| author_facet | Mohamed Ali, Jaafar Syed Sadeq, Tazkera |
| author_sort | Mohamed Ali, Jaafar Syed |
| building | IIUM Repository |
| collection | Online Access |
| description | 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. |
| first_indexed | 2025-11-14T15:27:49Z |
| format | Article |
| id | iium-29145 |
| institution | International Islamic University Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-14T15:27:49Z |
| publishDate | 2012 |
| publisher | Taylor's University |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | iium-291452013-02-26T02:39:26Z http://irep.iium.edu.my/29145/ Development of educational software for stress analysis of an aircraft wing Mohamed Ali, Jaafar Syed Sadeq, Tazkera TA349 Mechanics of engineering. Applied mechanics 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. Taylor's University 2012 Article PeerReviewed application/pdf en http://irep.iium.edu.my/29145/1/DEVELOPMENT_OF_EDUCATIONAL_SOFTWARE.pdf 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 |
| spellingShingle | TA349 Mechanics of engineering. Applied mechanics Mohamed Ali, Jaafar Syed Sadeq, Tazkera Development of educational software for stress analysis of an aircraft wing |
| title | Development of educational software for stress analysis of an aircraft wing |
| title_full | Development of educational software for stress analysis of an aircraft wing |
| title_fullStr | Development of educational software for stress analysis of an aircraft wing |
| title_full_unstemmed | Development of educational software for stress analysis of an aircraft wing |
| title_short | Development of educational software for stress analysis of an aircraft wing |
| title_sort | development of educational software for stress analysis of an aircraft wing |
| topic | TA349 Mechanics of engineering. Applied mechanics |
| url | http://irep.iium.edu.my/29145/ http://irep.iium.edu.my/29145/1/DEVELOPMENT_OF_EDUCATIONAL_SOFTWARE.pdf |