Educational Software for Stress Analysis of an Aircraft Fuselage

Abstract:

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A stress analysis software based on MATLAB graphical user interface (GUI) has been developed. The developed software can be used to estimate internal loads on a fuselage and to compute the stresses at any point along the length of the fuselage of a given aircraft. The generalized formulation allows user to perform stress analysis even on tapered fuselages. The software is expected to be a useful tool for effective teaching learning process of courses on aircraft structures and aircraft structural design.

Info:

Periodical:

Edited by:

Wu Fan

Pages:

3054-3062

DOI:

10.4028/www.scientific.net/AMM.110-116.3054

Citation:

J.S. M. Ali et al., "Educational Software for Stress Analysis of an Aircraft Fuselage", Applied Mechanics and Materials, Vols. 110-116, pp. 3054-3062, 2012

Online since:

October 2011

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Price:

$35.00

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