Aerodynamic Research on the Wing Design of a 3000 kg Hexa Tiltrotor eVTOL

This paper describes a design method for 3000 kg hexa tiltrotor eVTOL wings. According to this design method, this paper designs and optimizes the wing area and incidence angle using CFD technology, provides the optimal wing design scheme, and estimates the range of eVTOL based on CFD results. The results of the estimated range indicate that the wing designed according to the method in this paper can meet the requirements of eVTOL.