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.
· Advances in Science and Tech... · 0 citations