With the expansion of UAV mission, the traditional evaluation methods can not meet the requirements of modern mission design. In more and more airfoils, how to design and select airfoils suitable for mission requirements for aerodynamic design of aircraft is the primary problem that designers have to face. In this paper, aiming at the problems existing in the design of aerodynamic performance requirements of 40kg fixed-wing UAV, carbon fiber reinforced epoxy resin composite material was selected to design the wing in a flat configuration, and a fully carbon fiber UAV wing with a wingspan of two meters was designed. Then, the performance of the airfoil was evaluated through simulation analysis, providing a scientific basis for the selection of the airfoil for the aerodynamic design of UAV.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    A new tube-variant UAV wing design


    Contributors:
    Yuan, Xiaofang (editor) / Wu, Guanglei (editor) / Liang, Renjie (author) / Ren, Debin (author) / Han, Lei (author) / Liu, Miao (author)

    Conference:

    Third International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2023) ; 2023 ; Hangzhou, China


    Published in:

    Proc. SPIE ; 12722


    Publication date :

    2023-07-18





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Raptor-imitated variant wing

    TANG DI / HUANG XIPENG / CHE JINGQI et al. | European Patent Office | 2021

    Free access

    Foldable wing aircraft with wing variant structure

    GUI HAIFENG / JIANG SHANYUAN / ZHONG BOWEN et al. | European Patent Office | 2023

    Free access

    Variant mechanism of aircraft wing

    DU XIN / ZHANG SHENG / HUANG JIANGTAO et al. | European Patent Office | 2022

    Free access

    Variant flying wing type aircraft and variant method thereof

    WANG JIANMING / XIA XUANZE / ZHANG ZHENGHAO et al. | European Patent Office | 2021

    Free access

    From Tube and Wing to Flying Wing

    Torenbeek, Egbert | Wiley | 2013