Analysis of UAV wing load calculation

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.

書誌詳細
出版年:E3S Web of Conferences
第一著者: Lingjia Zhang
フォーマット: 論文
言語:英語
出版事項: EDP Sciences 2023-01-01
オンライン・アクセス:https://www.e3s-conferences.org/articles/e3sconf/pdf/2023/50/e3sconf_interagromash2023_02020.pdf