Experimental investigation of the effect of interface angle on mode-I fracture toughness in DCB laminates using digital image correlation

Journal Article (2025)
Authors

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)

Research Group
Group Pascoe
More Info
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Publication Year
2025
Language
English
Research Group
Group Pascoe
Bibliographical Note
Green Open Access added to TU Delft Institutional Repository ‘You share, we take care!’ – Taverne project https://www.openaccess.nl/en/you-share-we-take-care Otherwise as indicated in the copyright section: the publisher is the copyright holder of this work and the author uses the Dutch legislation to make this work public.@en
Volume number
319
DOI:
https://doi.org/10.1016/j.engfracmech.2025.110988
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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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