Kriging and Radial Basis Function Models for Optimized Design of UAV Wing Fences to Reduce Rolling Moment

<div>Diagram showing different angles of attack <i>s</i> in different fence positions: (a) 30% of the vortex diameter, (b) 50% of the vortex diameter, and (c) 70% of the vortex diameter.</div>

International Journal of Intelligent Systems

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Figure 13

Figure 13: Kriging and Radial Basis Function Models for Optimized Design of UAV Wing Fences to Reduce Rolling Moment 