Aerodynamic Optimization of a UAV Wing subject to Weight, Geometric, Root Bending Moment, and Performance Constraints

Table 3

Performance parameters of the baseline UAV.

	14.08
at	8°
at	15.52 m/s
at	127.46 Nm
	24.06 N
	39.45 m/s
at	-2.32°
	13.25
at	18°