• Title of article

    Low-velocity Impact Damage Analysis of Composite Laminates Using Self-adapting Delamination Element Method

  • Author/Authors

    Lipeng، نويسنده , , Wang and Ying، نويسنده , , Yan and Dafang، نويسنده , , Wu and Hao، نويسنده , , Wu، نويسنده ,

  • Issue Information
    روزنامه با شماره پیاپی سال 2008
  • Pages
    7
  • From page
    313
  • To page
    319
  • Abstract
    On the basis of a 2D 4-node Mindlin shell element method, a novel self-adapting delamination finite element method is presented, which is developed to model the delamination damage of composite laminates. In the method, the sublaminate elements are generated automatically when the delamination damage occurs or extends. Thus, the complex process and state of delamination damage can be simulated practically with high efficiency for both analysis and modeling. Based on the self-adapting delamination method, linear dy-namic finite element damage analysis is performed to simulate the low-velocity impact damage process of three types of mixed woven composite laminates. Taking the frictional force among sublaminations during delaminating and the transverse normal stress into account, the analytical results are consistent with those of the experimental data.
  • Keywords
    Delamination , Composite laminate , self-adapting delamination element method , Low-velocity impact
  • Journal title
    Chinese Journal of Aeronautics
  • Serial Year
    2008
  • Journal title
    Chinese Journal of Aeronautics
  • Record number

    2264731