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...
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Taylor's University
2012
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| Online Access: | http://irep.iium.edu.my/29145/ http://irep.iium.edu.my/29145/1/DEVELOPMENT_OF_EDUCATIONAL_SOFTWARE.pdf |
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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 |
| repository_type |
Digital Repository |
| institution_category |
Local University |
| institution |
International Islamic University Malaysia |
| building |
IIUM Repository |
| collection |
Online Access |
| language |
English |
| topic |
TA349 Mechanics of engineering. Applied mechanics |
| spellingShingle |
TA349 Mechanics of engineering. Applied mechanics Mohamed Ali, Jaafar Syed Sadeq, Tazkera Development of educational software for stress analysis of an aircraft wing |
| 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. |
| format |
Article |
| author |
Mohamed Ali, Jaafar Syed Sadeq, Tazkera |
| author_facet |
Mohamed Ali, Jaafar Syed Sadeq, Tazkera |
| author_sort |
Mohamed Ali, Jaafar Syed |
| title |
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_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_sort |
development of educational software for stress analysis of an aircraft wing |
| publisher |
Taylor's University |
| publishDate |
2012 |
| url |
http://irep.iium.edu.my/29145/ http://irep.iium.edu.my/29145/1/DEVELOPMENT_OF_EDUCATIONAL_SOFTWARE.pdf |
| first_indexed |
2023-09-18T20:42:46Z |
| last_indexed |
2023-09-18T20:42:46Z |
| _version_ |
1777409475534127104 |