A Multi-Scale Simulation Methodology for the Samarai Monocopter ?UAV

The Samarai UAV is a biologically-inspired monocopter, similar in its ight characteristics to the maple seed. It is essentially a single, asymmetric helicopter blade, powered by a tip propeller. Highdelity simulation of such a vehicle is challenging, but of great importance to e cient design. A multi-scale simulation methodology is presented, utilizing Computational Fluid Dynamics (CFD)-based predictions of the aerodynamic behavior, coupled to the more CPU-e cient blade element and free-wake vortex ring models. The resulting simulation is suitable for engineering analysis and design of monocopters, but nevertheless captures the relevant physical phenomena at low Reynolds number ight regime.