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Volume 40 Issue 2
Feb.  2014
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Journal of Beijing University of Aeronautics and Astronautics  > 2014  >  40(2): 188-192.
Yang Yongqiang, Ma Yunpeng, Wu Zheet al. Analysis of effect of interior pressure to deformation of inflatable wing with fluid-structure interaction analysis method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(2): 188-192. (in Chinese)
Citation: Yang Yongqiang, Ma Yunpeng, Wu Zheet al. Analysis of effect of interior pressure to deformation of inflatable wing with fluid-structure interaction analysis method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(2): 188-192. (in Chinese)
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Analysis of effect of interior pressure to deformation of inflatable wing with fluid-structure interaction analysis method

  • School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics,Beijing 100191, China

  • Received Date: 02 Jul 2013
  • Publish Date: 20 Feb 2014
    Abstract
  • Fluid-structure interaction (FSI)analysis of inflatable wing was carried out based on the ABAQUS-FLUENT FSI software. Distance-weighted average interpolation function was used to transfer aerodynamic pressure distribution between coupling interfaces. Deformation data was transferred using constant volume tetrahedron transformation method. Relationship among interior pressure, stiffness and buckling behavior of inflatable wing was obtained. Analog loading system of inflatable wing was established to validate the feasible of the optimization scheme. The results show that FSI method is applicable to make the deformation analysis of inflatable wing. The results of the FSI analysis and the analog loading test coincide to each other well.

     

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