• DocumentCode
    2266927
  • Title

    Delamination Growth of Foam Core Composite Sandwich Plate under Harmonic Dynamic Load

  • Author

    Ruixiang, Bai ; Shiyong, Sun ; Haoran, Chen

  • Author_Institution
    Dept. of Mech. Eng., Dalian Univ. of Technol., Dalian
  • Volume
    2
  • fYear
    2008
  • fDate
    20-22 Dec. 2008
  • Firstpage
    1011
  • Lastpage
    1015
  • Abstract
    In this paper, the delamination growth of sandwich plate with foam core and composite sheets under harmonic dynamic load is investigated by finite element method. The composite sheet is modeled as layered shell element considering first order shear effect, and the foam core is modeled as isotropic solid element; while for the bond line between sheet and core is simulated by using simple cohesive layer models with a bilinear constitutive relationship. Reference to previous experience, the most significant parameter GC is applied to tracing delamination growth. By some numerical examples, the behavior of dynamic delamination growth of sandwich plates is investigated.
  • Keywords
    composite materials; delamination; finite element analysis; foams; harmonics; plates (structures); sandwich structures; sheet materials; shells (structures); structural engineering; vibrations; cohesive layer models; composite sheets; delamination growth; finite element method; first order shear effect; foam core; harmonic dynamic load; isotropic solid element; layered shell element; sandwich plate; Aerodynamics; Delamination; Information technology; Intelligent structures; Intelligent vehicles; Sandwich structures; Solid modeling; Stress; Testing; Vehicle dynamics; FEM; composite sandwich plate; delamination; dynamic delamination growth;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Information Technology Application, 2008. IITA '08. Second International Symposium on
  • Conference_Location
    Shanghai
  • Print_ISBN
    978-0-7695-3497-8
  • Type

    conf

  • DOI
    10.1109/IITA.2008.173
  • Filename
    4739915