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...