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.
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Acknowledgment
The authors of this paper acknowledge the financial support by “Centre National pour la Recherche Scientifique et Technique” (CNRST) Rabat, Morocco.
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Bouchaâla, K., Driouch, I., Faqir, M., Ghanameh, M.F., Chouiyakh, H., Essadiqi, E. (2020). Numerical Prediction of Thickness Influence on the Aircraft Wing Design. In: Ezziyyani, M. (eds) Advanced Intelligent Systems for Sustainable Development (AI2SD’2019). AI2SD 2019. Advances in Intelligent Systems and Computing, vol 1104. Springer, Cham. https://doi.org/10.1007/978-3-030-36671-1_42
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DOI: https://doi.org/10.1007/978-3-030-36671-1_42
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