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Three-Dimensional (3D) aeromechanical analysis is carried out on the rotor blades of a 20 kg Mars Hexacopter. The objectives are to understand the aeroelastic behavior of its unique and ultra-thin low-Reynolds number and high-Mach number blades and study the interactions of structures, aerodynamics, and control moments in the Martian atmosphere.

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This page is a summary of: Aeromechanical Analysis of a Next-Generation Mars Hexacopter Rotor, Journal of Aircraft, November 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c036739.
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