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M. K. Abbas

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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

The combined results demonstrate that implementing a one-way aero-structural coupling approach better predicts loading accuracy and the resultant structural response, giving a more reliable basis for preliminary aircraft wing design.

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

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