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Slipstream Deformation of a Propeller-Wing Combination Applied for Convertible UAVs in Hover Condition

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Figure

Figure 2: Convertible UAV Cyclone hovering with negative flap deflection
Figure 5: Flow speed measurement
Figure 8: Comparison of axial velocity distribution at differ- differ-ent rotation speeds
Figure 9: Geometry relations to determine slipstream centre
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