Effects of Wind Disturbance on the Aerodynamic Performance of a Quadrotor MAV during Hovering

Figure 18

Pressure contour of blade tip with horizontal wind disturbance: (a) 2.5 m/s—1500 RPM; (b) 4.0 m/s—1500 RPM; (c) 2.5 m/s—1700 RPM; (d) 4.0 m/s—1700 RPM; (e) 2.5 m/s—2100 RPM; (f) 4.0 m/s—2100 RPM.

(a)

(b)

(c)

(d)

(e)

(f)