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

<div>A diagram showing different angles of attack <i>s</i> in different positions (A, B, C, and O) of the fence. (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 19

Figure 19: Kriging and Radial Basis Function Models for Optimized Design of UAV Wing Fences to Reduce Rolling Moment 