Educational Software for Stress Analysis of an Aircraft Fuselage

J.S. Mohammed Ali; Izyan Liyana Mustafa Kamal; Nurhuda Ismail

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

Paper Titles

Analysis of Radiative Heat Flux for Nozzle Flow
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Comprehensive Study of Typical Metamodel Methods Applied in Aircraft Multidisciplinary Design Optimization
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Investigation of Various Parametric Geometry Representation Methods for Airfoils
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Interpretive Structural Modeling (ISM) of Bolted Joint Subjected to Dynamic Loosening under Soft Foot Condition
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Educational Software for Stress Analysis of an Aircraft Fuselage
p.3054

Physical Simulation on Temperature and Pressure Fields during Steamflooding through Horizontal Wells in Heterogeneous Reservoir
p.3063

Elastic Exploring Law Analysis of the Deep Vuggy Reservoir
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Modeling and Analysis of the Current Generated by Compensatory Anticathode in the Electric Fields Protection of Ship
p.3074

The Special Chao and Singularity in a Simple Traffic Model
p.3080

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 110-116Educational Software for Stress Analysis of an...

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.

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Periodical:

Applied Mechanics and Materials (Volumes 110-116)

Pages:

3054-3062

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.110-116.3054

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Online since:

October 2011

Authors:

J.S. Mohammed Ali, Izyan Liyana Mustafa Kamal, Nurhuda Ismail

Keywords:

Aircraft Fuselage, Educational Software, MATLAB, Stress Analysis

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