헥사콥터의 제자리 비행 시 후류 특성에 관한 수치해석 A Numerical Analysis of Wake Characteristics in Hovering Flight of Hexa-copter
한국기계기술학회지
(韓國機械技術學會誌)
제24권 제6호
(2022.12)
pp.1113-1119
pp.1113-1119
한국기계기술학회
(Korean Society of Mechanical Technology)
초록
In this study, a numerical analysis was performed as steady-state analysis to investigate the effect of interference between the propellers of the hexa-copter. As the distance increases, there is little change in thrust, but when a propeller close to the reference propeller rotates, it was confirmed that the thrust decreased due to the interference effect. Unsteady state analysis was performed to confirm the influence of the hexa-copter fuselage. If there is a fuselage, the thrust was predicted to increase by about 4.97% due to the ground effect. If the design parameters are established considering the effect of the fuselage of the hexa-copter, it is expected to be used for basic design and application design in the future.
저자