Structural Analysis of a Transport Aircraft Wing-Reference-Cited by-同舟云学术

Structural Analysis of a Transport Aircraft Wing

Published:2021-03-05 Issue:1 Volume:13 Page:3-9
ISSN:2247-4528
Container-title:INCAS BULLETIN
language:en
Short-container-title:INCAS BULLETIN

Author:

ABBAS Yassir¹,ELSONNI Tariq²,ABDULMAJID Abdul Aziz³,KHALAFALLH Alnazir³,ALNAZIR Mohammed³

Affiliation:

1. Aeronautical Engineering Department, Engineering College, Karary University, Khartoum, Sudan, yasirabas75@hotmail.com

2. International College of Science and Technology, Khartoum, Sudan

3. Aeronautical Engineering Department, Engineering College, Karary University, Khartoum, Sudan

Abstract

In this study the procedures of structural analysis of a typical transport aircraft wing has been followed. The wing model has been drawn using CATIA® V5; this model consists of several structural components such as spars, ribs and skin. The model has been exported into structural analysis software ANSYS® 2016. Stresses, strains, deformations and safety factors were obtained for the model. It is found that the obtained stresses caused by the aerodynamic loads on the wing are within the design structural limits where the failure by yield or buckling has not been occurred

Publisher

INCAS - National Institute for Aerospace Research Elie Carafoli

Subject

Aerospace Engineering,Control and Systems Engineering

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