Educational software for stress analysis of idealized closed thin walled sections
Aerospace structures are typical semi-monocoque structures that are made up of thin-walled closed section reinforced with stiffeners. Stress analysis of such closed thin-walled structures which are statically indeterminate is tedious and time consuming. An educational software which can aid students...
| Main Authors: | , , , |
|---|---|
| Format: | Proceeding Paper |
| Language: | English English |
| Published: |
2018
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/68442/ http://irep.iium.edu.my/68442/1/68442_Educational%20Software%20for%20Stress%20Analysis.pdf http://irep.iium.edu.my/68442/2/68442_Educational%20Software%20for%20Stress%20Analysis-tentative.pdf |
| _version_ | 1848786942887460864 |
|---|---|
| author | Syed Mohamed Ali, Jaffar Nur Fadhila, Hasna Makame, Burhani Riyadh, Miah Mohammed |
| author_facet | Syed Mohamed Ali, Jaffar Nur Fadhila, Hasna Makame, Burhani Riyadh, Miah Mohammed |
| author_sort | Syed Mohamed Ali, Jaffar |
| building | IIUM Repository |
| collection | Online Access |
| description | Aerospace structures are typical semi-monocoque structures that are made up of thin-walled closed section reinforced with stiffeners. Stress analysis of such closed thin-walled structures which are statically indeterminate is tedious and time consuming. An educational software which can aid students in stress analysis of such idealized thin-walled closed sections has been developed. The software enables students to select different types of wing torsion box sections with stiffeners, which may be subjected to bending, shear or torsional loads and evaluate the resulting stresses on it. The software allows the student to idealize a selected twin spar unsymmetrical wing section with multiple booms under multiple loads. Results from this software have been validated against the results in the literature. The software has been developed using MATLAB with graphical user interface (GUI) which is very user friendly. The software is expected to be a very useful tool for effec-tive teaching learning of courses on thin-walled structures and automotive/aircraft structures. |
| first_indexed | 2025-11-14T17:17:03Z |
| format | Proceeding Paper |
| id | iium-68442 |
| institution | International Islamic University Malaysia |
| institution_category | Local University |
| language | English English |
| last_indexed | 2025-11-14T17:17:03Z |
| publishDate | 2018 |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | iium-684422018-12-21T08:27:09Z http://irep.iium.edu.my/68442/ Educational software for stress analysis of idealized closed thin walled sections Syed Mohamed Ali, Jaffar Nur Fadhila, Hasna Makame, Burhani Riyadh, Miah Mohammed TL Motor vehicles. Aeronautics. Astronautics Aerospace structures are typical semi-monocoque structures that are made up of thin-walled closed section reinforced with stiffeners. Stress analysis of such closed thin-walled structures which are statically indeterminate is tedious and time consuming. An educational software which can aid students in stress analysis of such idealized thin-walled closed sections has been developed. The software enables students to select different types of wing torsion box sections with stiffeners, which may be subjected to bending, shear or torsional loads and evaluate the resulting stresses on it. The software allows the student to idealize a selected twin spar unsymmetrical wing section with multiple booms under multiple loads. Results from this software have been validated against the results in the literature. The software has been developed using MATLAB with graphical user interface (GUI) which is very user friendly. The software is expected to be a very useful tool for effec-tive teaching learning of courses on thin-walled structures and automotive/aircraft structures. 2018 Proceeding Paper NonPeerReviewed application/pdf en http://irep.iium.edu.my/68442/1/68442_Educational%20Software%20for%20Stress%20Analysis.pdf application/pdf en http://irep.iium.edu.my/68442/2/68442_Educational%20Software%20for%20Stress%20Analysis-tentative.pdf Syed Mohamed Ali, Jaffar and Nur Fadhila, Hasna and Makame, Burhani and Riyadh, Miah Mohammed (2018) Educational software for stress analysis of idealized closed thin walled sections. In: International Conference on Aviation Technology and Management (ICATEM2018), 12th-14th Sept. 2018, Kuala Lumpur. (Unpublished) |
| spellingShingle | TL Motor vehicles. Aeronautics. Astronautics Syed Mohamed Ali, Jaffar Nur Fadhila, Hasna Makame, Burhani Riyadh, Miah Mohammed Educational software for stress analysis of idealized closed thin walled sections |
| title | Educational software for stress analysis of idealized closed thin walled sections |
| title_full | Educational software for stress analysis of idealized closed thin walled sections |
| title_fullStr | Educational software for stress analysis of idealized closed thin walled sections |
| title_full_unstemmed | Educational software for stress analysis of idealized closed thin walled sections |
| title_short | Educational software for stress analysis of idealized closed thin walled sections |
| title_sort | educational software for stress analysis of idealized closed thin walled sections |
| topic | TL Motor vehicles. Aeronautics. Astronautics |
| url | http://irep.iium.edu.my/68442/ http://irep.iium.edu.my/68442/1/68442_Educational%20Software%20for%20Stress%20Analysis.pdf http://irep.iium.edu.my/68442/2/68442_Educational%20Software%20for%20Stress%20Analysis-tentative.pdf |