Composite material wing structure optimization method based on topological optimization

The invention discloses a composite material wing structure optimization method based on topological optimization, and the method comprises the steps: carrying out the preliminary optimization through employing a topological optimization method based on a finite element model of a target structure,...

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Bibliographic Details
Main Authors TIAN XIAO, HOU JUNPING, KANG JIANXIONG, LI NA, CAO YAQI, GUO WEIXING
Format Patent
LanguageChinese
English
Published 26.01.2024
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