Flight Endurance Increasing Technology of New Energy UAV Based on a Strut-Braced Wing

Table 1

Aerodynamic shape parameters of Dandelion I.

Major component	Parameter name	Value and unit
Wing	Wingspan	6150 mm
	Wing chord	423 mm
	Install angle	2.5°
	Dihedral angle	3°
	Sweep angle	0°
	Root-tip ratio	1
Tail	Horizontal tail span	1260 mm
	Horizontal tail chord	253 mm
	Horizontal tail root-tip ratio	1
	Vertical tail span	450 mm
	Vertical tail cord	260 mm
Fuselage	Cross-section height	250 mm
	Cross-section width	250 mm
	Length	1342.96 mm