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Ground effect on aerodynamic characteristics of flapping-wing micro air vehicles

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In this research, the program is written in FORTRAN programming language by using OpenMP library for parallel computing. It was found that the ground effect is the most significant when the flapping-wing micro air vehicle is hovering with a reduction in the lift force when the distance from the center of mass of the flapping-wing micro air vehicle to the ground is below 0.05 m. For forward flight, this effect tends to decrease as the flight speed increases. |

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