AIAA 2000-0896 Simulation of the Dynamics of Micro Air Vehicles
نویسندگان
چکیده
A finite element flow solver based on unstructured grids is employed for studying the aerodynamic characteristics of Micro Air Vehicles. Inviscid and viscous flow simulations were performed for two different Micro Air Vehicles developed at NRL. Lift and drag force variations were computed for a range of flow angles and control surface angles. The Baldwin-Lomax turbulence model was employed for turbulent flows. An actuator disk model was used to study the effect of the propeller flow.
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