Paper Title:
Educational Software for Stress Analysis of an Aircraft Fuselage
  Abstract

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
Chapter
Chapter 14: Modeling, Analysis, and Simulation of Manufacturing Processes
Edited by
Wu Fan
Pages
3054-3062
DOI
10.4028/www.scientific.net/AMM.110-116.3054
Citation
J.S. M. Ali, I. L. M. Kamal, N. Ismail, "Educational Software for Stress Analysis of an Aircraft Fuselage", Applied Mechanics and Materials, Vols. 110-116, pp. 3054-3062, 2012
Online since
October 2011
Export
Price
$32.00
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