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

Table 4

Performance parameters of baseline UAV and the optimum UAVs.

	Baseline UAV	Case 1	Case 2	Case 3
	14.08	30.79	18.95	18.21
(°)	8	5.56	5.69	6.44
(m/s)	15.52	11.97	13.41	14.41
(Nm)	127.46	249.4	127.3	127.4
	24.06	37.64	19.41	21.8
	39.45			39.45
(°)	-2.32			-5.3
	13.25			12.58
(°)	18			17.86