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Numerical Prediction of Thickness Influence on the Aircraft Wing Design

  • Kenza BouchaâlaEmail author
  • Ismail Driouch
  • Mustapha Faqir
  • Mohamad Fathi Ghanameh
  • Hajar Chouiyakh
  • Elhachmi Essadiqi
Conference paper
  • 25 Downloads
Part of the Advances in Intelligent Systems and Computing book series (AISC, volume 1104)

Abstract

This paper deals with the numerical prediction of the Von Mises and the displacement of the swept back wing can withstand under different pressure conditions. In this study ABAQUS was used as a finite element software, with the help of CAD software Catia V5 to model and assemble each of the 3D wing components.

Keywords

ABAQUS Aircraft wing CATIA modelling Displacement Finite element 

Notes

Acknowledgment

The authors of this paper acknowledge the financial support by “Centre National pour la Recherche Scientifique et Technique” (CNRST) Rabat, Morocco.

References

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    Barbero, E.J.: Finite Element Analysis of Composite Materials using Abaqus. CRC Press, Boca Raton (2013)CrossRefGoogle Scholar
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    Material Data Sheet Aluminum 7475-T761. Aerospace Specification Metals (2015)Google Scholar
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    Toan, V., Hoang, H.: Simplified design of a commercial aircraft wing made of carbon fiber (2015)Google Scholar
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    Jweeg, M.J., AL-Tornachi, P.D.S.J., Abid-Aun, S.H.: Optimization of light weight aircraft wing structure. J. Eng. Dev. 12, 1 (2008)Google Scholar

Copyright information

© Springer Nature Switzerland AG 2020

Authors and Affiliations

  • Kenza Bouchaâla
    • 1
    • 2
    Email author
  • Ismail Driouch
    • 1
  • Mustapha Faqir
    • 1
  • Mohamad Fathi Ghanameh
    • 1
    • 3
  • Hajar Chouiyakh
    • 1
  • Elhachmi Essadiqi
    • 1
  1. 1.AERO School of Engineering, LERMA Lab.International University of RabatSala el JadidaMorocco
  2. 2.Mohammadia School of Engineers, ITACS Lab.Mohammed V UniversityRabatMorocco
  3. 3.Department of Mechanical Conception-Faculty of Mechanical and Electrical EngineeringDamascus UniversityDamascusSyria

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