E3S Web of Conferences (Jan 2023)

Analysis of UAV wing load calculation

  • Lingjia Zhang

DOI
https://doi.org/10.1051/e3sconf/202341302020
Journal volume & issue
Vol. 413
p. 02020

Abstract

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According to the existing wing structure design cases, design a simple model of the UAV wing according to the engineering needs, and use the flow-solid coupling function of the ansys finite element analysis software to calculate the working load of the wing structure.