EPJ Web of Conferences · 2013 · 15 citations · 0 references
EngineeringFluid MechanicsWinglet DesignStructural OptimizationUnsteady FlowAeronauticsAircraft Design ProcessWing DesignWing AerodynamicsNaca 0012Isolated WingDesignExternal AerodynamicsApplied AerodynamicsAerostructureAerospace EngineeringExperimental StudyAeroelasticityAerodynamicsAutomotive Aerodynamics
In the present study, an experimental study is presented for a flow around an isolated wing equipped by a winglet and profiled with Naca 0012. Several cases of winglets were tested according to the angle ß: 0°, 55°, 65°and 75°. For all these cases at a velocity of 20, 30 and 40 meters per second, wind tunnel tests are performed and compared for different angles of incidence. It is observed that the aerodynamic performance of the winglet with β= 55° differ favorably for positive angle of incidence compared for other cases.