Table 1. The specification of UAM model

Specification Value
Fuselage Length (m) 4.12
Height (m) 1.64
Width (m) 2.04
Wing Span (m) 15.03
Chord (m) 1.59
Area (m2) 26.35
Aspect ratio 6.36
Airfoil NACA 2208
Lift fan Diameter (m) 2.7
Hub diameter (m) 0.54
Beta 3/4(°) 15.49
CT 0.4
CP 0.6
Activity factor 151.54
Pusher fan Diameter (m) 2.7
Hub diameter (m) 0.54
Beta 3/4(°) 15.49
CT 0.4
CP 0.6
Activity factor 151.54