Recently, agricultural drones have been widely used for precise agricultural control. In the case of drone control, improved coverage and reduced drift potential of chemical sprays are of major concern, and this is greatly influenced by the downwash flow characteristics formed by the rotor blades. In this study, the mean and turbulent flow characteristics of the downwash flow generated by a single blade of a four-sided agricultural control drone were quantitatively evaluated. The blade radius used to generate the downwash flow was 370 mm, and the measurement position was normalized using this length. Downwash flow was measured at 400 mm × 400 mm at 10-mm intervals in the X-Y plane and for 6 measurement planes at 100-mm intervals along the Z-direction. The rotational speed of the blade was set to 2,000, 2,500, and 3,000 rpms and the velocity components were dimensionless expressed using the blade tip velocity (VBtip) corresponding to this rotational speed. The velocity of downwash flow was measured using CTA-type hot-wire anemometry with an X-type probe, and object were collected at a sampling rate of 30 kHz for turbulence characteristics analysis. The mean velocity, vorticity distribution, turbulence intensity, and Reynolds stress of the fluctuation velocity were quantitatively measured. From extensive experimental works, it was revealed that a high axial velocity is formed at a specific position (r/Lb=0.4-0.8) along the blade length. The radial velocity shows an asymmetric distribution in the plane close to the blade, and the tangential velocity is higher in the central part of the downwash flow than in the region of a high axial and negative radial velocity. An asymmetric spiral rotational flow with low axial velocity and low-pressure distribution exists inside the downwash flow due to the shear flow, and the influence of the driving motor almost disappears at the axial position (Z/Lb ~ 1). In addition, a flow visualization experiment was carried out, using a high-speed camera, CCD camera and a seeding generator to capture the position, rotation speed, and vorticity intensity of the three blade tip vortices from 0 degrees to 180 wake age at 1,000, 1,500, 2,000, 2,500, 3,000 rpms.