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R. Saran

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Sep 2026

Iso-mass finite element assessment of ZE10A magnesium alloy as a lightweight alternative to AA5086 in thin-walled UAV wing structures

Reducing structural mass while maintaining stiffness and stability margins is a key requirement in thin-walled UAV wings. Magnesium alloys offer a density advantage over aluminum alloys, but their lower elastic modulus requires assessment in stability-driven designs. This study evaluates ZE10A magnesium alloy as a ligh...

R. Saran, E. L. Schneider, Charles Amaral de Jesus Cordeiro et al. · 0 citations

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