In-Plane Compressive Behaviour of Stiffened Thin-Skinned CFRP Panels with a Stress Concentrator  
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Soutis-Fleck Fracture Model
Applied to 'EDAVCOS' Panel

  • Loading Condition:
    Compressive Displacement Control applied parallel to stiffeners
  • Boundary Conditions:
    Sides parallel to stiffeners are free. Remaining Sides are fully clamped.
  • 15 J impact damage in skin bay replaced by an open hole. This model provides the stress distribution adjacent to the hole.
  Stable Fracture FE model – Compressive loading in vertical direction.
  • Loading Condition:
    Tensile Displacement Control.
  • Crack is introduced by disconnecting appropriate nodes along crack line.
  • The models created for each crack length provide the strain energy levels in each state.
  Unstable Fracture FE model – Tensile loading in vertical direction.
 
     
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