Experimental investigation of the effect of interface angle on mode-I fracture toughness in DCB laminates using digital image correlation
Linlin Deng (COMAC Beijing Aircraft Technology Research Institute)
Liu Liu (COMAC Beijing Aircraft Technology Research Institute)
John- Alan Pascoe (TU Delft - Group Pascoe)
R.C. Alderiesten (TU Delft - Group Alderliesten)
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Abstract
This study investigates the Mode-I fracture toughness of laminates with varying interface angles. A method for identifying crack tip location using grayscale characteristic parameters in DIC is proposed. The findings demonstrate that both initial and steady-state fracture toughness exhibit a bilinear relationship with interface angle. A cohesive constitutive model incorporating the interface angle was developed and integrated into a double cantilever beam finite element model, predicting delamination propagation behavior that was highly consistent with experimental results. Numerical analysis suggests that zigzag cracks may improve fracture toughness before steady-state toughness is achieved, with peak toughness correlating to the length of the zigzag cracks.
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