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 |
| Summary: | 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. |
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