Browsing by Author "Xiang, Jinwu"

Browsing by Author "Xiang, Jinwu"

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  • Adaptive control of a nonlinear aeroelastic system 
    Li, Daochun; Xiang, Jinwu; Guo, Shijun J. (Elsevier Science B.V., Amsterdam., 2011-07-01)
    Aeroelastic two-dimensional wing section with both trailing-edge (TE) and leading-edge (LE) was investigated in this paper through numerical simulation in time domain. Structural stiffness and damping in pitch degree of ...
  • Aeroelastic dynamic response and control of an airfoil section with control surface nonlinearities 
    Li, Daochun; Guo, Shijun J.; Xiang, Jinwu (Elsevier Science B.V., Amsterdam, 2010-10-31)
    Nonlinearities in aircraft mechanisms are inevitable, especially in the control system. It is necessary to investigate the effects of them on the dynamic response and control performance of aeroelastic system. In this ...
  • Buckling and post-buckling of a composite C-section with cutout and flange reinforcement 
    Guo, Shijun J.; Li, Daochun; Zhang, Xiang; Xiang, Jinwu (Elsevier, 2013-12-31)
    This paper presents an investigation into the effect of cutout and flange reinforcement on the buckling and post-buckling behaviour of a carbon/epoxy composite C-section structure. The C-section having a cutout in the web ...
  • A review of modelling and analysis of morphing wings 
    Li, Daochun; Zhao, Shiwei; Da Ronch, Andrea; Xiang, Jinwu; Drofelnik, Jernej; Li, Yongchao; Zhang, Lu; Wu, Yining; Kintscher, Markus; Monner, Hans Peter; Rudenko, Anton; Guo, Shijun; Yin, Weilong; Kirn, Johannes; Storm, Stefan; De Breuker, Roeland (Elsevier, 2018-06-20)
    Morphing wings have a large potential to improve the overall aircraft performances, in a way like natural flyers do. By adapting or optimising dynamically the shape to various flight conditions, there are yet many unexplored ...