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 allows performing stress ana...

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Bibliographic Details
Main Authors: TAZKERA SADEQ, J. S. MOHAMMED ALI
Format: Article
Language:English
Published: Taylor's University 2012-06-01
Series:Journal of Engineering Science and Technology
Subjects:
Online Access:http://jestec.taylors.edu.my/Vol%207%20Issue%203%20June%2012/Vol_7_3_322_338_J.%20S.%20MOHAMMED%20ALI.pdf