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Mokdad Hayawi Rahman

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Open access Oct 2026

Integrated one-way aero-structural analysis of an aircraft wing using a MATLAB-based panel method and finite element analysis

In this work, an integrated aero-structural methodology is presented, combining a MATLAB panel-method aerodynamic solver with ANSYS finite-element analysis to predict the performance of a tapered NACA 2412 wing. The pressure distribution obtained from the panel method gave good agreement with CFD data, with a maximum d...

M. K. Abbas, T. Elsonni, Mokdad Hayawi Rahman et al. · 0 citations

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