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
  • Linear Buckling Analysis results showed that the model’s stiffness was comparable to the real panel.
Linear Buckling analysis showed that the panel buckled at 407kN. Moiré Images of the EDAVCOS panel subjected to uniaxial compressive loading. The panel buckled at 452kN.
 
     
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