%0 Journal Article
%T DEVELOPMENT OF EDUCATIONAL SOFTWARE FOR STRESS ANALYSIS OF AN AIRCRAFT WING
%A J. S. MOHAMMED ALI
%A TAZKERA SADEQ
%J Journal of Engineering Science and Technology
%D 2012
%I Taylor's University
%X 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.
%K Education
%K Software
%K Stress analysis
%K Aircraft wings
%K MATLAB
%U http://jestec.taylors.edu.my/Vol%207%20Issue%203%20June%2012/Vol_7_3_322_338_J.%20S.%20MOHAMMED%20ALI.pdf