Trapezoidal cellular support structure applied to flexible telescopic sandwich skin of morphing wing

被引：0
|
作者：
Shen, Yuan [1 ]
Ang, Haisong [1 ]
Liu, Weidong [1 ]
机构：
[1] State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
来源：
Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica | 2015年 / 32卷 / 03期
关键词：
D O I：
10.13801/j.cnki.fhclxb.20140917.001
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：815 / 822
相关论文
共 24 条
  • [21] RETRACTION: Optical fiber shape sensing of polyimide skin for a flexible morphing wing (Retraction of Vol 56, Pg 9325, 2017)
    Sun, Guangkai
    Li, Hong
    Dong, Mingli
    Lou, Xiaoping
    Zhu, Lianqing
    APPLIED OPTICS, 2022, 61 (06) : 1413 - 1413
  • [22] Multi-disciplinary Optimization of Composite Sandwich Structure for an Aircraft Wing Skin Using Proper Orthogonal Decomposition
    Park, Chanwoo
    Kim, Young Sang
    JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2019, 47 (07) : 535 - 540
  • [23] RETRACTED: Optical fiber shape sensing of polyimide skin for a flexible morphing wing (Retracted article. See vol. 61, pg. 1413, 2022)
    Sun, Guangkai
    Li, Hong
    Dong, Mingli
    Lou, Xiaoping
    Zhu, Lianqing
    APPLIED OPTICS, 2017, 56 (33) : 9325 - 9332
  • [24] A Shear-Sliding Rigid-Flexible Coupled Skin Variable-Sweep Wing Design and Heat-Fluid-Structure Multifield Coupling Analysis
    Xiao, Hong
    Guo, Hongwei
    Li, Mingqi
    Zhang, Yu
    Liu, Rongqiang
    Tao, Jianguo
    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2023, 2023
123