Rotary wing aerodynamics have historically been widely investigated due to the large number of applications of this discipline in several fields of engineering. A deep knowledge of the main phenomena related to rotary wing aerodynamics such as dynamic stall or blade vortex interactions (BVI) is essential for the design of novel VTOL aircraft configurations as tiltrotors or compounds. In recent years, the great interest and development efforts devoted to new designs of unconventional urban air mobility VTOL aircraft based on electric distributed propulsion have focused on rotor–rotor and rotor–body aerodynamic interactions.
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