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Lightweight Design of Four-rotor UAV Fuselage based on Topology Optimization
Process Technology | 更新时间：2024-01-15

    • Lightweight Design of Four-rotor UAV Fuselage based on Topology Optimization

    • Engineering Plastics Application   Vol. 51, Issue 2, Pages: 60-66(2023)

    • DOI：10.3969/j.issn.1001-3539.2023.02.010    

      CLC： TB324

    • Received：01 December 2022，

      Published：10 February 2023

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  • Li Heng，Yan Wenkai，Chen Yihao，et al. Lightweight design of four-rotor UAV fuselage based on topology optimization[J]. Engineering Plastics Application，2023，51(2)：60-66. DOI： 10.3969/j.issn.1001-3539.2023.02.010.

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