2024
DOI: 10.1155/2024/4108121
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Kriging and Radial Basis Function Models for Optimized Design of UAV Wing Fences to Reduce Rolling Moment

Mohammad Hossein Moghimi Esfand-Abadi,
Mohammad Hassan Djavareshkian,
Afshin Madani

Abstract: In the present study, the effects of the wing fence on the wing tip vortices and control surfaces located at the tip of the wing in a flying wing aircraft have been investigated using a numerical method. For the size of the fences, the average dimensions extracted from the wing tip vortices at different angles of attack are used. The basic determining parameter is the rolling torque coefficient, which is tried to be shown by employing a parametric study of the flow behavior in different situations of fence pla… Show more

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