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

Table 5

Geometric properties of the wings of the baseline UAV and the optimum UAV wings.

	Baseline UAV	Case 1	Case 2	Case 3
	0.12	0.08	0.08	0.092
	0.4	0.524	0.566	0.494
	0.04	0.08	0.08	0.063
	0.45	0.386	0.586	0.596
	0.45	0.2	0.2	0.2
	4	8	4.578	4.524
	1.8	2.34	1.8	1.8