• Title of article

    Compression, flexure and shear properties of a sandwich composite containing defects

  • Author/Authors

    Mouritz، A.P. نويسنده , , Thomson، R.S. نويسنده ,

  • Issue Information
    روزنامه با شماره پیاپی سال 1999
  • Pages
    -262
  • From page
    263
  • To page
    0
  • Abstract
    The mechanical properties of a sandwich composite containing interfacial cracks or impact damage are compared when loaded in edgewise compression, flexure or shear. The composite is made from glass fibre reinforced polymer (GFRP) laminate skins over a core of foamed poly vinyl chloride (PVC), and this sandwich material is used in some naval minehunting ships. The properties are reduced with increasing interfacial crack or impact damage length, but only when the defects cause a change in the failure mode, which is dependent on the load state. The principal failure modes under the different load states are compared. The properties are also dependent on the severity of impact damage, with low energy damage to the skin having a smaller effect on stiffness and strength than high energy impacts which damage both the skin and foam core. The implications of these findings on the structural integrity of a minehunting ship made from GFRP/PVC foam sandwich composite is discussed. © 1999 Elsevier Science Ltd. All rights reserved.
  • Keywords
    Failure mode maps , Honeycomb sandwich panels
  • Journal title
    COMPOSITE STRUCTURES
  • Serial Year
    1999
  • Journal title
    COMPOSITE STRUCTURES
  • Record number

    4090