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

Table 1

Effect of , , and to the results and .

			(%)	(%)	(s)
41	0.05	0.01	0	0	3007.7
31	0.05	0.01	0.4	1.1	2532.9
31	0.1	0.01	0.4	1.1	1096.2
31	0.2	0.01	0.4	1.1	519.3
31	0.2	0.05	5.9	1.1	418.5
31	0.2	0.1	11.2	1.0	414.3
31	0.2	0.2	15.2	0.9	347.6