• DocumentCode
    525270
  • Title

    Analysis of aerocyst cell inflation deformation based on finite element method

  • Author

    Li Jun ; Tang Zhen-nan ; Wang Zi-liang ; Li Ai-ping

  • Author_Institution
    Coll. of Aerosp. Eng. & Mech., Tongji Univ., Shanghai, China
  • Volume
    1
  • fYear
    2010
  • fDate
    25-27 June 2010
  • Abstract
    Inflatable structures shape accuracy and stability are a key factor of the wing structural design. The article introduced the application of finite element analysis in inflatable structure form-finding,analyzed the influence of the inflatable aerocyst cellular construction parameters to the inflation deformation,has attributed its relative relations with curves and the function,and further studied the relations between the construction weight and inflation deformation with the parameters variation.
  • Keywords
    aerospace components; design engineering; finite element analysis; plastic deformation; structural engineering; aerocyst cell; finite element method; inflatable structure formfinding; inflation deformation; shape accuracy; shape stability; wing structural design; Aerodynamics; Aerospace engineering; Automotive components; Biological materials; Biomembranes; Building materials; Educational institutions; Finite element methods; Mechanical engineering; Shape control; finite element method; function; inflatable structure; inflation deformation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computer Design and Applications (ICCDA), 2010 International Conference on
  • Conference_Location
    Qinhuangdao
  • Print_ISBN
    978-1-4244-7164-5
  • Electronic_ISBN
    978-1-4244-7164-5
  • Type

    conf

  • DOI
    10.1109/ICCDA.2010.5541064
  • Filename
    5541064