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Analysis of UAV wing load calculation

E3S Web of Conferences (2023) 413
DOI: 10.1051/e3sconf/202341302020
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Abstract

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.

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APA

Lingjia, Z. (2023). Analysis of UAV wing load calculation. In E3S Web of Conferences (Vol. 413). EDP Sciences. https://doi.org/10.1051/e3sconf/202341302020

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