Volume 26 Issue 3
Jun.  2011
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HU Jiang-bo, LIANG Xian-zhu, ZHANG Cheng, CHEN Xiang-ming, YANG Yu. Study on Structure Design and Manufacture of High Load-weight Ratio Composite Wing Model[J]. Development and Application of Materials, 2011, 26(3): 37-40. DOI: 10.19515/j.cnki.1003-1545.2011.03.011
Citation: HU Jiang-bo, LIANG Xian-zhu, ZHANG Cheng, CHEN Xiang-ming, YANG Yu. Study on Structure Design and Manufacture of High Load-weight Ratio Composite Wing Model[J]. Development and Application of Materials, 2011, 26(3): 37-40. DOI: 10.19515/j.cnki.1003-1545.2011.03.011
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Study on Structure Design and Manufacture of High Load-weight Ratio Composite Wing Model

  • 1. Beijing Aeronautical Manufacturing Technology Research Institute, Beijing 100024, China;

  • 2. Aircraft Strength Research Institute of China, Xi'an 710065, China

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  • Available Online: March 27, 2024
    Graphical Abstract
    • Abstract
  • In accordance with the outline of the wing model given and in order to achieve high load-weight ratio of the wing， three layouts of wing structure are presented. One of them， the straight-beam layout， is determined after analysis of simulation of FEM and manufacture process. The forming process has been advanced， which is proved feasible and reasonable through the forming-quality verification and load test.
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