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Parametric Optimization of Load Bearing Elements for Composite Wing of an Unmanned Aerial Vehicle
2021
MATEC Web of Conferences
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This paper describes the optimizing results of structural elements of the composite wing of an unmanned aerial vehicle. The thickness and composite lay-up structure of load-bearing elements and wing skin are determined using the ANSYS software package. The optimal structure is presented using the Pareto set method of the "ideal center" basing on four criteria: minimum mass, deflection, normal stress, and maximum safety factor of the wing. Verification calculations were carried out to determine
doi:10.1051/matecconf/202134603093
fatcat:6amzruiyjvh53nfrsicesx53em