Abstract:The rotary wing and the flapping wing technology for the MAVs (Micro Air Vehicle) demand the studies of unsteady aerodynamic effects on the vehicles performing near the ground. In this study, a fast and robust numerical method based on the general formulae for the lift and propulsive forces, acting on a heaving-plunging airfoil, induced by a vortex sheet and its ground image, is developed and implemented. The Keldish-Lavrentiev series expansion of the Kernel function is employed to find the effect of the image… Show more
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